US20120192158A1 - Model Based Verification Using Forward and Reverse Traversal of Variable Time Line - Google Patents

Model Based Verification Using Forward and Reverse Traversal of Variable Time Line Download PDF

Info

Publication number
US20120192158A1
US20120192158A1 US13/302,546 US201113302546A US2012192158A1 US 20120192158 A1 US20120192158 A1 US 20120192158A1 US 201113302546 A US201113302546 A US 201113302546A US 2012192158 A1 US2012192158 A1 US 2012192158A1
Authority
US
United States
Prior art keywords
time
values
variables
variable
diagram
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US13/302,546
Inventor
Carlo Amalfitano
Timothy Stockton
Christopher Marot
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Certon Software Inc
Original Assignee
Certon Software Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Certon Software Inc filed Critical Certon Software Inc
Priority to US13/302,546 priority Critical patent/US20120192158A1/en
Assigned to Certon Software Inc. reassignment Certon Software Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: STOCKTON, TIMOTHY
Publication of US20120192158A1 publication Critical patent/US20120192158A1/en
Assigned to Certon Software Inc. reassignment Certon Software Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: AMALFITANO, CARLO, STOCKTON, TIMOTHY, MAROT, CHRISTOPHER
Abandoned legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/36Preventing errors by testing or debugging software
    • G06F11/3668Software testing
    • G06F11/3672Test management
    • G06F11/3684Test management for test design, e.g. generating new test cases

Definitions

  • This application relates to a verification and debugging technique allowing forward and reverse time traversal of variable values for signal-processing-type programming and model-based verification.
  • Software that is critical to flight operations (Class A) is tested with extreme care. Usually this software belongs to a special category of coding, which can be generally described as signal processing.
  • the software receives input signals from a variety of real-world sources, such as a pilot adjusting a control yoke, rudder pedals, and/or throttle controls, altimeter, attitude indicator, airspeed indicator, magnetic compass, or other flight instrumentation, analog to digital converters (A/D), etc., and continuously processes such signals at a steady rate, fixed frames or whenever necessary.
  • the software produces output signals in the form of commands or warnings, via Digital to Analog converters (D/A).
  • the user by himself or herself or possibly jointly with the manufacturer of the actual hardware, often referred to as a black box, that runs the software prepares a set of clearly defined and understandable specifications and requirements, which define the processes inside the black box.
  • a black box that runs the software prepares a set of clearly defined and understandable specifications and requirements, which define the processes inside the black box.
  • a set of test cases and test procedures are independently prepared in order to verify that the black box performs properly. That is, the black box does everything it is required to do, and only what it is required to do.
  • test cases that apply combinations of Boolean values to the input of the element under test, and state what results should be expected.
  • test cases are translated into test procedures.
  • the test procedures are then run to collect actual results, and compare the actual results with the expected results.
  • a common methodology for such procedures is to force values into the code, referred to as stabbing, and extract output values from some intermediate place in the code process.
  • the method discussed above only proves that the black box has the correct collection of elements, not that the elements are correctly connected. In other words, the verification process discussed above does not prove that the black box works properly end-to-end. It, therefore, does not prove that the black box, as a whole, will behave as intended.
  • the generation of such test procedures at the black box level is difficult for several reasons.
  • the variables used for inputs to a component, or block may not be the same as the black box level real world inputs, and the outputs from the component, or block, may not be real world outputs from the black box. Therefore, the inputs to the element under test must be “demoted” to real world inputs, and the outputs from the element under test must be “promoted” to real world outputs.
  • the verification process requires the test engineer to generate one test procedure for each targeted component, diagram, or block of components.
  • the test procedure must be of a duration that addresses all timing issues, achieves the desired inputs using a combination of real world input values, and also generates real world outputs that are representative, in a detectable, unique way, of the targeted component outputs.
  • the test procedure is complete when all the aspects of the targeted component are tested under the specified guidelines, such as modified condition/decision coverage, exhaustive, etc.
  • one way to generate independent expected outputs is to provide and run an alternative code in the black box.
  • This is often referred as a “model,” but it could be just an alternative instantiation of the code, such as code independently produced by another team.
  • the expected results are produced using a different compiler, a different hardware platform, and a different operating system than the black box.
  • a currently available method of performing reconciliation use the debugging features of two compilers in an integrated design environment (IDE), for example, compiling the model code side-by-side with the black box code.
  • IDE integrated design environment
  • This method allows only “forward” debugging, meaning that both compilers must be stopped at the same point in the respective codes so that the user can look at values held by variables and data structures. The user then move to the next break point and again looks at values held by variables and data structures, and so on.
  • the reconciliation process is difficult and may take very long time.
  • Reconciliation is particularly long and difficult if the model is written using visual techniques, such as Simulink®, and/or if the input data to the black box cannot be provided faster than real time—it is normally provided much slower than real time.
  • Simulink® is a registered trademark of MathWorks, Inc., of 3 Apple Hill Drive, Natick, Mass. 01760.
  • the user may wait 10 minutes between break points, the point at which he may be able to investigate mismatching values, just to learn that the process must be started anew.
  • a layer of code that “wraps around” the model code and at each execution of the code (at each frame of signal processing), saves the names of the variables explicitly (i.e. in ASCII format or any readable format with the name as it appears on the specifications, and not as a memory address) and saves also all the values assumed by that variable at each frame evaluation.
  • some other information will be saved, such as the type of variable, the time at which it was saved, etc., depending on the project.
  • the variables for which the values are saved are all the variables in the system or a subset of them or even a superset (including special variables desirable for “setting the stage” of the test).
  • This innovative technique can be applied to any programming related to signal processing, i.e. to any program that receives a set of inputs and produces outputs at intervals, such as model-based verification as in DO 178B. Nevertheless, similar techniques could be expanded to any Integrated Development Environment (IDE).
  • IDE Integrated Development Environment
  • the innovative technique described herein allows the user to select a point in time (for example using a slider or moving the mouse on a timeline) and inspect the values assumed by one or more selected variables (also clicked with mouse actions). Note that the user can go forward and reverse in the time selection on any value, and repeat at will, with immediate visualization of the results.
  • the time required for this technology to display any value at any time is miniscule in comparison to alternative techniques.
  • this technique requires the program (the Test Procedure or the “model”) to run entirely through once (without break points or debug settings) to completion, so that all the values can be saved.
  • the variables are shown in a convenient order (possibly in alphabetical order), and a small window allows a user to type any portion of a variable name the user intends to select. Matching variable names are then automatically highlighted and selected. Values for the selected variables can be automatically shown at the time selected by the mouse sliding back and forth on the canvas. If only one variable (or a few variables) are selected, there is enough room on the screen to show the values on a sliding window that shows, in the center, the value at the corresponding selected time, and also shows values for the same variable some frames before and some frames after the selected time.
  • the variables are shown in a window with a “scroll box”, and the values are shown for the desired time (frame) selection for the variables visible in the scroll box.
  • the selected (or all) variable(s) may be shown in graphical format.
  • the arrangement of the values is particularly important in model based verification, because “flag shaped” boxes can be displayed attached to points of interest on a diagram showing the desired functionality of the code. Since the flag-shaped boxes show the values of the signal at the spot indicated on the diagram at the time selected by the user moving the mouse on the canvas timeline, the debugging of a model-based becomes fast and easy.
  • An automated program process is then run, for example, code which is “wrapped around” the Model Code
  • the process is run in a way such that, for each SimVar at each DataSim input time, all outputs can be stored.
  • the pseudocode for an example program process can be as follows:
  • input signals are associated with input variable names, and then an input variable holds in a timeline all the desired input signal values for that variable.
  • the collection of input values are transferred to memory using the pointers associated with the explicit variable names. Then, one computational event (frame) is evaluated and the Real World outputs are stored.
  • a timeline is made of 100 seconds and 100 samples per second.
  • the timeline for each variable thus contains 10,000 values.
  • the above pseudo-code would be repeated 10,000 times to create a “SimRun”, but the execution time is not much more that executing the Black Box program itself, given that what is added is just moving data from one location in memory to another, for the tracked variables.
  • the above process is executed ONCE and then all the data are ready to be displayed for any selected time (frame).
  • the showing portion of the program or “user interface” can then produce a “canvas” where a user can manipulate an input device such as a mouse or a touchscreen to select a time or times and variables to be viewed (perhaps adding a cross-hair), and data are then visualized (in any form) from the SimRun Timeline.
  • an input device such as a mouse or a touchscreen
  • data are then visualized (in any form) from the SimRun Timeline.
  • FIG. 1 is a high level operations flow diagram.
  • FIG. 2 illustrates a main window of the user interface.
  • FIGS. 3-8 illustrate several example diagrams of signal processing components of a Black Box used as part of a Demo project.
  • FIGS. 9-14 illustrate various ways to verify certain diagrams.
  • FIG. 15 illustrates how to set IntelliPoints.
  • FIG. 16 is another verification view.
  • FIG. 17 illustrates verification of a timer.
  • FIG. 18 is a state diagram for timer verification.
  • FIGS. 19-21 are other timer verification diagrams.
  • FIG. 1 is a high level operations flow diagram of an example embodiment of a Model-Based Verification Application 100 .
  • Model-Based Verification Application 100 is made of several components.
  • the Model Core 105 provides many of the features of the Model-Based Verification Application 100 , such as generating input signal timelines using Intelligent Points, all graphical rendering and displaying of signals and corresponding signal processing components or blocks of connected components (also referred to hereafter as the “diagrams”), debugging capabilities, file name and file input/output (I/O) services.
  • the UNITSCD (Specification Control Drawings) 110 is a code unit where all the information pertaining to the diagrams is stored.
  • the information can include the devices, ASCII names of variables, the positions of flags, and constants on the diagram visual representations.
  • the VARSANDBODIES 115 enables the functionality of each diagram. It also enables the functionality of the complete Black Box under test by connecting together or “stitching” two or more of the diagrams that make up the Black Box.
  • the VARSANDBODIES 115 is made up of calls to a library of components with standard behavior, or in some cases custom behavior.
  • the library components can include, but are not limited to, Boolean logic gates, such as, OR gates, AND gates, and NOT gates, and other signal processing functions, such as delay timers, and various filters.
  • the VARSANDBODIES 115 also provides all the variables of the Black Box in static memory.
  • This structure allows this same Model Core 105 to be re-used in different projects.
  • New custom components can be added to the library of components as necessary. Using minimal additional resources, the custom components can be carried on as legacy elements in projects that do not use them.
  • the UNITSCD 110 and VARSANDBODIES 115 code units are typically new and unique for each project. Thus, they typically are developed for a specific project, and cannot be re-used in a different project. These code units can be considered to belong to a customer of the user.
  • the VARSANDBODIES 115 needs to be compiled for performance, while the UNITSCD 110 is a database-like set of information.
  • Alias Table 120 is a computer file, such as an Excel® file that contains information regarding names of variables used in the actual code, i.e., the code under test. (Excel is a registered trademark of Microsoft Corporation, One Microsoft Way, Redmond, Wash. 98052.) Such information can further include minimum and/or maximum limitations for values, granularity or decimation/digitalization properties, diagram stitching information, and other names in use. Information regarding other variable names in use is especially useful when there is redundancy, and/or inconsistency in the signal naming scheme among and between model code and actual code.
  • Diagram Bitmaps 125 are a visual representation of the diagrams.
  • the Diagram Bitmaps 125 can be a screen shot, or scan, of a diagram. While visual representations can be generated from the file that stores the diagram in native format, such as Visio®, Simulink®, or similar tool, it is preferred to use a bitmap file, because there are no possible errors in the interpretation of the native-mode files. In other words, what you see is what you get with bitmap files.
  • CMOD Files 130 are computer files, such as Excel® files, that contain visual information, and environment or harness parameters about a specific test.
  • the CMOD Files 130 contain only the “Intelligent Points” that allow the creation of complete test files in conjunction with the Model 101a/b.
  • Test Cases 135 are a collection of computer files, such as Excel® files, which are related to a single diagram.
  • the columns represent all the input variables and output variables of the related diagram, and each row represents the inputs, and expected outputs, for each and every processing step.
  • the Test Case 135 files contain all of the I/O variables, input values, and expected output values for each step of time along a timeline.
  • Test Procedures 140 are a collection of files, such as Excel® files, which have columns representing Real World input values and output values.
  • the input values contain all the initial condition values for variables. That is, Test Procedure 140 files contain all the Real World values that set the stage for the test, including the values for all the variables that have non-nominal values—even if they do not change during the test.
  • the Real World output variables represented are a set of manually selected variables pertinent to a specific test. Each row represents input values and expected output values, for every time step.
  • Each Test Procedure 140 is a companion to a Test Case 135 , in the sense that the Test Procedure 140 will faithfully generate the Test Case 135 data for the related diagram, when the Real World input values traverse the diagram. In other words, when the Real World input values are completely processed according to a Test Procedure 140 , the Test Case 135 data will be generated for the associated diagram.
  • the Hardware (or Rig) 145 is the actual physical equipment against which the Model 101 is verified. Test Procedures 140 are submitted to the Hardware 145 to produce Actual Results, which are then fed back to the Model 101 and/or stored in record-keeping or version control systems 155 , such as Subversion® or ClearCase®. (Subversion is a registered trademark of CollabNet, Inc., 8000 Marina Blvd., Suite 600, Brisbane, Calif. 94005; and ClearCase is a registered trademark of Atria Software, Inc., 24 Prime Park Way, Natick, Mass. 01760.)
  • Model-Based Verification Application 100 The purpose of the Model-Based Verification Application 100 is to ascertain that each block in the Back Box, such as one or more selected components or diagrams, produces the intended functionality.
  • the verification process is a complex function that depends on device type, signal type, required verification procedures, and several other parameters. Verification must sometimes also comply with applicable standards 170, such as DO178 as applied to flight code, and perhaps other custom requirements.
  • each device can be verified by specifying a combination of Intelligent Points 175 (also referred to herein as “IntelliPoints”).
  • An Intelligent Point is a command for a variable to assume a value, or a signal type, from one point in time until the point in time of the next Intelligent Point 175 .
  • an Intelligent Point 175 dictates the signal type for an input variable, and therefore input values, for a period of processing time along a time line.
  • the simplest form of input variable signal is a linear interpolation between the two points, but other signal can be created in accordance with the selected attributes of the Intelligent Point 175 .
  • Intelligent Points 175 in a particular Model 101 may vary depending on many considerations, normally a very small set of Intelligent Points 175 is sufficient for a particular verification. For example, a method for verification of a DelayOn device requires only four Intelligent Points 175 to generate the Boolean input values necessary to verify Persistency and Expiration tests. However, the Intelligent Points 175 must be carefully and appropriately set in time. For other variables more points may be required to promote the output signal to a visible Real World signal, using a promotion process.
  • the selecting or setting of Intelligent Points 175 can be achieved via a trial-and-error manual process, aided by the Model's 101 recalculation of all signals when a point is moved.
  • Useful to selecting of Intelligent Points 175 is a real-time recalculation, which allows the user to graphically see the implications on all signals when an Intelligent Point 175 is modified in time, value or signal type, or another Intelligent Point 175 is added.
  • FIG. 2 illustrates a user interface 200 for specifying various parts of the Model 101.
  • the main window of the user interface 200 is organized in tabs 205 . All options are preferably immediately visible with no hidden drop-down menus. All folder names 210 are always visible, and can be typed or browsed. Subsets of file names 215 can be selected by using a standard Windows mask. All parameters are saved in a local file for each PC, or user. All visible lists of files and produced tables can be saved in Excel® format for re-use.
  • the stitched Model 101 consumes all the Real World input variables and produces all the Real World output variables.
  • the list of all the input variables can be impractical to maintain in some projects, therefore the Model 101 resorts to Intelligent Points 175 for Virtual Real World input variables.
  • Virtual Real World input variables it is intended as a variable that does not exist as a real world input variable, that may have a similar name to a Real World input variable, and has the purpose of setting a number of Real World input variables to the desired value or values, according to rules.
  • the setting of a variable carried by a triple-redundant ARINC bus typically requires setting the value of 12 input variables; 3 values for each of the following: Data, Activity, Parity, and Sign/Status Matrix (SSM).
  • SSM Sign/Status Matrix
  • an input variable can assume a value in degrees inside the Black Box, or even inside a particular diagram, but has a real world input variable value in radians, or Sines and Cosines, the Virtual Real World input variable is set in degrees, and the Model 101 adjusts the input values to Sines and Cosines accordingly.
  • the Virtual Variable can be set to any value, but the Model 101 limits the Real World input values according to the specified minimum and maximum values in the Alias table 120 (shown in FIG. 1 ) and only produces values that match the actual granularity of the input values, i.e., the digitized or decimated values, so that the variables internal to the Black Box can only assume values that can be carried through the physical hardware. This is useful so that model-computed expected results can exactly match Black-Box computed actual results.
  • variable values are carried to the Black Box model via communications channels or buses.
  • a bus or channel has a width in bits.
  • the bus may also have a 10-bit width.
  • a 10-bit A/D is connected to a sensor that measures Vertical Speed Accelerations (VSA) in gravitational-force (Gs). Further assuming that the aircraft in which the VSA is installed is designed to operate between ⁇ 3 and +7 Gs, and that the device will disintegrate if the acceleration exceeds the range between ⁇ 6 and +14 Gs.
  • the sensor is capable of providing data values between ⁇ 20.48 and +20.44 Gs.
  • the Alias table 120 would carry the information about range and granularity for this variable.
  • the Model 101 would use the Alias table 120 to create input values only in accordance with the range and granularity.
  • the variable input can assume values from ⁇ 20.48 to +20.44 Gs, in 0.04 increments, the values outside of the range between ⁇ 6 and +14 Gs are meaningless, because, in the real world the VSA sensor would be destroyed. It would useful that a project have a limiting layer of code that ensures that all input variable values are meaningful operational values.
  • FIG. 3 is an example of an analog limiting and combining diagram 301 a, for which the input variable ranges are specified, contained within the Black Box.
  • the tabs 370 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • VAR_S_A 302 can range from a MAX_SA 303 value of +21.0 down to a MIN_SA 305 of ⁇ 8.0.
  • VAR_S_B 312 ranges from a MAX_SB 313 value of +7.0 down to a MIN_SB 315 of ⁇ 7.0
  • VAR_S_C ranges from a MAX_SC 323 value of +10.0 down to a MIN_SC 325 of ⁇ 10.0.
  • the limiters 350 produce the Real World output variables, VAR_S_A_LIM 307 , VAR_S_B_LIM 317 , and VAR_S_C_LIM 327 .
  • the combiner 360 use Real World output variables VAR_S_A_LIM 307 , VAR_S_B_LIM 317 , and VAR_S_C_LIM 327 to produce VARS_S_AB 319 and VAR_S_AC 329 .
  • the input variable values ranges, MAX_SA 303 , MIN_SA 305 , MAX_SB 313 , MIN_SB 315 , MAX_SC 323 , and MIN_SC 325 are shown in green.
  • Window pane 301 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as input/internal/output (I/N/O), visibility, decimals, color, line width (LW), scale/bias, actual value, and variable name, for the diagram 301 a.
  • I/N/O input/internal/output
  • LW line width
  • scale/bias actual value
  • variable name variable name
  • FIG. 4 illustrates another diagram 401 a inside the Black Box containing different types of components, such as DelayOn 405 , Boolean gates 406 , 407 , and a decision making comparator 408 .
  • the tabs 470 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • the flag-shaped rectangles, with a numeric or Boolean value inside, or flags 402 are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams.
  • the components DelayOn 405 , Boolean gates 406 , 407 , and decision making comparator 408 operate in accordance with their respective function and connections, or stitching, on the values associated with VAR_B_Z 411 , VAR_B_Y 412 , VAR_B_X 413 , VAR_B_W 419 , VAR_S_U 415 , and VAR_S_T 416 to produce output variables VAR_B_ZOR 421 , VAR_B_WXY 422 , and VAR_B_TU 423 .
  • Window pane 401 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 401 a.
  • FIG. 5 illustrates yet another example diagram 501 a containing a Differentiator (S) 551 , Integrator (1/S) 552 , Limited Integrator 553 and a couple of First-Order filter components 554 .
  • the tabs 570 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • the flags 502 are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams.
  • the components Differentiator (S) 551 , Integrator (1/S) 552 , Limited Integrator 553 and couple of First-Order filter components 554 operate in accordance with their respective functions and connections on the values associated with input variables VAR_S_A_LIM 307 , VAR_S_B_LIM 317 , and VAR_S_C_LIM 327 to produce output variables VAR_S_A_DIFF 521 , VAR_S_B_INTEG 522 , VAR_S_B_INTLIM 523 , VAR_S_C_FILT 524 and VAR_S_C_FOFILT 525 .
  • Window pane 501 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 501 a.
  • FIG. 6 exemplifies yet another example diagram 601 a that has four different Second-Order filters 650 .
  • the tabs 670 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • the six constants 653 the numbers shown in green, define the response characteristics of each Second-Order filter 450 .
  • the parameters of the Second-Order filters 450 are shown in the S-domain, but Z-domain parameters can also be used.
  • the flags 602 are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams.
  • the Second-Order filter components 650 operate in accordance with their respective functions, including their respective response characteristics, and their connections on the values associated with input variable VAR_S_C_LIM 327 to produce output variables VAR_S_C_HPFILT 621 , VAR_S_C BPFILT 622 , VAR_S_C_BSFILT 623 , and VAR_S_C_SOFILT 624 .
  • Window pane 601 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 601 a.
  • FIG. 7 shows another example diagram 701 a a special type of Second-Order filter, a Notch Filter 750 .
  • the tabs 770 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • the six constants 753 the numbers shown in green, define the response characteristics of the Notch filter 750 .
  • the parameters of the Notch filter 750 are shown in the S-domain, but Z-domain parameters can also be used.
  • the Notch filter component 750 operates in accordance with its respective function, that is filtering according to its response characteristics, and connections, on the values associated with input variable VAR_S_C_LIM 327 to produce output variables VAR_S_C_NOTCH 721 .
  • Window pane 701 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 701 a.
  • FIG. 8 illustrates a diagram 801 a in which analog and Boolean (digital) variables are processed for presentation to a Real World output layer.
  • the purpose of this diagram is to exercise the stitching between diagrams and components and the promotion process of moving virtual variables to the Real World.
  • the tabs 870 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box.
  • the flags 802 are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams.
  • switches 850 and mixer 851 operate in accordance with their respective functions and connections on the values associated with input variables VAR_S_A_DIFF 521 , VAR_B_ZOR 421 , VARS_S_B_INTEG 522 , VAR_S_B_INTLIM 523 , VAR_S_C_FILT 524 , VAR_B_WXY 422 , VAR_S_C_FILT 524 VAR_S_C_FOFILT 525 and VAR_B_TU 423 to produce output variables VAR_S_AB_OUT 821 , VAR_S_BC_OUT 822 , and VAR_S_C_OUT 823 .
  • Window pane 801 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 801 a.
  • FIG. 9 is an example of a timeline plot of signals used for verification of the diagram with limiters 301 a (shown in FIG. 3 ).
  • the canvas 901 a depicts a 30 second timeline of signals 910 , 920 , and 930 .
  • the window pane 901 b on the left contains a list of all variable inputs (here, all Virtual) and all variables output to the Real World.
  • the three waveforms of signals 910 , 920 , and 930 each have an amplitude that exceeds the limits of the values for the input variables corresponding to the respective limiters 350 (shown in FIG. 3 ). Therefore, the signals 910 , 920 , and 930 are useful to verify, at least partially, the performance of the limiters 350 .
  • FIG. 10 is another diagram illustrating an alternate example approach to verification of the diagram 301 a with limiters ( FIG. 3 ).
  • Canvas 1001 a depicts a 30 second timeline of signals 1010 , 1020 , and 1030 .
  • the three waveforms, signals 1010 , 1020 , and 1030 are obtained suing a few IntelliPoints 1050 .
  • a single IntelliPoint 1050 defines each of the periodic sinusoidal waveforms 1010 (colored purple) and 1030 (red) by setting their respective frequencies in Hertz, and amplitudes.
  • the waveform signal 1020 (green) is generated by linear interpolation between the adjacent IntelliPoints 1050 in a set of four IntelliPoints 1050 .
  • FIG. 11 illustrates an example verification of the limiter diagram 301 a ( FIG. 3 ) in another way.
  • the values for the input variables and output variables are plotted as a function of time on the canvas 1101 a.
  • window pane 110 ab the user can inspect the variables local to the diagram 301 a at the same time as he or she sets the Real World input values.
  • the effect of the limiters 350 is obvious from the chopping of peaks and troughs shown in the output signals 1114 , 1115 , 1116 , 1117 , and 1118 generated from the sinusoidal waveform input signals 1111 , 1112 , and 1113 .
  • Dragging an IntelliPoint to reposition it along the canvas has an immediate effect on both windows, allowing the user to gauge the verification effort.
  • FIG. 12 illustrates an example verification of the limiter diagram 301 a ( FIG. 3 ).
  • Canvas 1201 a depicts a 30 second timeline of signals 1210 , 1220 , and 1230 .
  • the three waveforms, signals 1210 , 1220 , and 1230 are obtained suing a few IntelliPoints 1050 .
  • a single IntelliPoint 1250 defines each of the periodic sinusoidal waveforms 1210 (colored purple) and 1230 (red) by setting their respective frequencies in Hertz, and amplitudes.
  • the waveform signal 1220 (green) is generated by linear interpolation between the adjacent IntelliPoints 1250 in a set of four IntelliPoints 1050 .
  • FIG. 12 illustrates an example verification of the limiter diagram 301 a ( FIG. 3 ).
  • Canvas 1201 a depicts a 30 second timeline of signals 1210 , 1220 , and 1230 .
  • the three waveforms, signals 1210 , 1220 , and 1230 are obtained
  • FIG. 13 depicts another example diagram 1301 a, which show the values of all the variables at that time in the flags 1302 .
  • the flags 1302 containing variable values at the specified time step, are over-imposed to the bitmap of the diagram 1301 a.
  • example diagram 1300 is displayed at the same time as the verification display 1200 ( FIG. 12 ). Other features of the figure have been previously described.
  • FIG. 14 illustrates another example embodiment of a step in a verification method.
  • a Real World output variable that unequivocally represents the diagram output variable. This can be achieved through a process called promotion, in which a signal is promoted towards the output. It is useful to unequivocally represented a signal that is the output variable of a diagram, but is an intermediate variable, i.e., a non-Real World output of the Black Box. This can be accomplished by navigating to diagrams downstream of the diagram under test (i.e., signal processing functions that occur later in the Model 101 process) and selecting suitable variables that represent the original signal as the output.
  • the diagram under test is diagram 301 a (shown in FIG.
  • an intermediate variable is VAR_S_AB_OUT 1410 .
  • Canvas 1401 a depicts a 30 second timeline of signals 1010 , 1020 , and 1030 .
  • Window pane 1402 displays a data for intermediate variable is VAR_S_AB_OUT 1410 , including values and time increments for each processing frame number and the frame number.
  • FIG. 15 illustrates a preferred graphical user interface (GUI) 1501 for selecting or setting IntelliPoints.
  • GUI graphical user interface
  • the choice of the parameters for the IntelliPoints can be simple and intuitive.
  • the following commands are preferably used in a graphical view of input variable values as a function of time, such as illustrated in FIG. 14 : a left-click of a mouse allows a user to drag-and-drop the IntelliPoint to a new location; a center-click deletes the IntelliPoint; and, a right-click opens a window, such as for the GUI 1501 , where the user can set a variety of parameters.
  • a variety of attributes can be selected to create functions for input variable values, such as normal (i.e., linear interpolation) 1510 , frequency 1511 , pulses 1512 , square wave 1513 , saw wave 1514 , hold value (i.e., set to a constant) 1515 , and frequency increment 1516 .
  • normal i.e., linear interpolation
  • frequency 1511 i.e., pulses 1512
  • square wave 1513 i.e., square wave 1513
  • saw wave 1514 i.e., set to a constant
  • hold value i.e., set to a constant
  • frequency increment 1516 i.e., set to a constant
  • certain other IntelliPoint parameters will become available to the user.
  • FIG. 16 illustrates the CMOD files contents 1600 for the verification of a relatively complex diagram. While the CMOD file is shown in Excel®, the user never has to manually operate within Excel® program.
  • the CMOD file 130 and 1600 represents a complete Test Procedure.
  • FIG. 17 illustrates a typical diagram 1701 a for timer verification containing a set of logical rules. It should be understood that such rules can vary depending upon project requirements.
  • the Boolean logic is normally tested using Modified Condition/Decision Coverage (MCDC).
  • MCDC Modified Condition/Decision Coverage
  • FIG. 19 illustrates an example method of verifying the timer on Boolean logic diagram 1701 a ( FIG. 17 ).
  • the setting of four IntelliPoints 1950 is sufficient to verify the timer.
  • Window pane 1901 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 1901 a.
  • FIG. 20 illustrates an example verification method of the diagram 1701 a ( FIG. 17 ) in another way.
  • the canvas 2001 a in window 2000 shows the variables related to the diagram under test only, such as VAR_BZ 2010 , VAR_BY 2020 , VAR_BX 2030 , VAR_BW 2040 , VxB 1 2050 , VAR_B_ZOR 2060 , VAR_B_WXY 2070 , and VAR_B_TU 2080 .
  • FIG. 21 illustrates verification of the diagram 700 with Notch Filter ( FIG. 7 ).
  • the notch filter is verified by appropriately selecting a few IntelliPoints.
  • One IntelliPoint sets a variable-frequency waveform 2110
  • another IntelliPoint sets a square wave (impulse response)
  • another IntelliPoint sets a frequency 2115 tuned to the expected “notch.”
  • the amplitude of the response characterizes the filter parameters.
  • the Test Case results in an Excel® file with 1500 rows (30 frames at 20 millisecond per frame).
  • the Test Cases generated using appropriately selected IntelliPoint verify all the relevant and necessary variables at all signal processing frames.
  • the Test Procedures compare expected results, those produces by the Model, and actual results, those produced by the Black Box, for all the variables at each and every frame, leaving no uncertainties regarding random, unexpected variable values or wrong stitching between diagrams.
  • the IntelliPoints are similar to fractals in that IntelliPoints expand to a lengthy and complex Test Case and Test Procedure files. This expansion process is relatively simple and the Test Cases and Test Procedures are automatically generated by the Model. While the Test Case and Test Procedure files are lengthy and complex, at the same time, the IntelliPoints are humanly understandable and settable, with the aid of the backward and forward timeline traversal debugging and visualization features of the Model.
  • An example embodiment of the method has been proven successful in a project with 200 complex diagrams and 6,000 variables, while still providing reasonably approximate real time feedback when moving IntelliPoints.
  • the 500 CMOD files having an average of 20 IntelliPoints each, produced four giga bytes (4 GB) of Excel® Test Cases and Test Procedures in about 6 hours of batch processing on a medium-powered PC.
  • the complete verification process produces only IntelliPoints that verify the desired specifications for all components.
  • each Intelligent Point only requires a few minutes of user attention. This is particularly useful to save time in the event that the requirements change; the user needs only to add or modify a few Intelligent Points, after which the system can re-compute all expected results for all diagrams.
  • the batch process that re-computes output variable values at all times is particularly useful because a change in requirements, or a change in a diagram, can significantly alter the expected results, and is very difficult to predict. Then, the batch process may produce then correct verification, which perhaps is incomplete.
  • the verification of a component is complete only when the component is fully exercised according to specification. However, an incomplete verification is still useful if the expected results match the actual results.
  • the completion of the verification may be achieved in steps, for example, by adding Intelligent Points, to the existing Test Cases and Test Procedures.
  • the above described forward and reverse timeline traversal debugging technique is more than simply moving a mouse back and forth on a timeline. It is a complex balance of programming resources allocation. It provides the user with the perception that all the variables in all the diagrams are immediately recalculated for any change to the Intelligent Points and other parameters, and that all the values are immediately available at the time frame where the mouse is positioned on the timeline. This perception of real-time availability is useful to enable the interactive interface allowing the user to easily and quickly set IntelliPoints for verification. Test Case is manually generated, and the generation process is aided by the real-time feedback of the expected results, immediately available to the user to explore for each device and each variable at any time interval along the timeline.
  • the above described forward and reverse timeline traversal debugging technique stores all the values for a complete timeline run within a few seconds, but allows the user to select a time, for example by using mouse movement or using arrow keys, and immediately—within milliseconds—see the values for all the variables.
  • the first feature is the fact that the program tracks which diagram the user is viewing. The user can only look at one diagram at a time. Thus, when the user changes a diagram tab, a two second time for recalculation is acceptable.
  • the Model Core only needs to lift the values of the variables the user can see from static memory, at end of each computational frame. This can be done without disturbing the model code execution or adding cycles to it.
  • the data is quickly accessed and copied from the variable's values, at each computational frame, are stored sequentially in memory, for immediate access, with access via frame number. This allows the corresponding values to be immediately displayed when the engineer selects any time corresponding to a computational frame. While it is true that all the data could be saved at each frame, it would require many gigabytes of memory for a large project, and the program would be slow for a variety of other reasons, such as memory paging.
  • the data related to the I/O variables that the user can actually “see” on the timeline are stored in a memory array for each frame of execution along the timeline.
  • the data related to the I/O variables that the user can see may include either the flag over the variable name in the diagram bitmap or the variable plotted with appropriate bias and colors.
  • the model core After the data has been stored, when the user moves the mouse on the timeline plot, the model core only displays all the variables that the user can see on the diagram under being viewed. Since this process typically takes a very short time for a reasonable diagram, for example, less than 100 milliseconds after the mouse settles, the user perceives that the program responds immediately.
  • variable names are immediately reported.
  • the user needs only to select the time (i.e. processing frame) with a single mouse motion—for any frame in the timeline—moving the cross-hair on the canvas.
  • pre-consume variables that are produced later during the computational chain.
  • a variable assumes two different values during a single computational frame, such as when an output signal is fed back to some input.
  • pre-consumption is solved by storing the value of the intermediate, non-Real World I/O variables at the time when the diagram under test is executed, in the order of execution chain, and not at the end of the computational frame. This feature can also be bypassed, if the need arises.

Abstract

A technique for debugging of a program model (or the debugging and reconciliation of two independent software model instantiations) with the perception of immediate showing of values assumed by all variables at any selected time, by permitting a user to move a selected test point in a forward and reverse direction along a time line, without recalculating the model each time the test point is moved. This is achieved by running the program model once and then saving all the variable values in memory, the values associated with the explicit name of the pertaining variable.

Description

    RELATED APPLICATION(S)
  • This application claims the benefit of U.S. Provisional Application No. 61/416,152, filed on Nov. 22, 2010, U.S. Provisional Application No. 61/416,153, filed on Nov. 22, 2010, U.S. Provisional Application No. 61/458,406, filed on Nov. 23, 2010, U.S. Provisional Application No. 61/458,410, filed on Nov. 23, 2010 and U.S. Provisional Application No. 61/481,973, filed on May 3, 2011. The entire contents of the referenced applications are hereby incorporated by reference.
  • TECHNICAL FIELD
  • This application relates to a verification and debugging technique allowing forward and reverse time traversal of variable values for signal-processing-type programming and model-based verification.
  • PROBLEMS WITH THE EXISTING ART
  • Several categories of software require very careful verification. In some cases the verification is mandated by government agencies, with strict requirements and procedures. This is typical, but not limited, to aircraft flight code and critical medical equipment code. For instance, the Federal Aviation Administration requires that software used in aeronautical applications be tested according with DO 178B standards.
  • Software that is critical to flight operations (Class A) is tested with extreme care. Usually this software belongs to a special category of coding, which can be generally described as signal processing. In other words, the software receives input signals from a variety of real-world sources, such as a pilot adjusting a control yoke, rudder pedals, and/or throttle controls, altimeter, attitude indicator, airspeed indicator, magnetic compass, or other flight instrumentation, analog to digital converters (A/D), etc., and continuously processes such signals at a steady rate, fixed frames or whenever necessary. The software produces output signals in the form of commands or warnings, via Digital to Analog converters (D/A).
  • The user, by himself or herself or possibly jointly with the manufacturer of the actual hardware, often referred to as a black box, that runs the software prepares a set of clearly defined and understandable specifications and requirements, which define the processes inside the black box. In the verification process, a set of test cases and test procedures are independently prepared in order to verify that the black box performs properly. That is, the black box does everything it is required to do, and only what it is required to do.
  • In the past, a typical approach to verification has been to list the requirements to an “atomic” level, the smallest possible testable unit, such as an AND or OR logic gate, write test cases that apply combinations of Boolean values to the input of the element under test, and state what results should be expected. Such test cases are translated into test procedures. The test procedures are then run to collect actual results, and compare the actual results with the expected results. A common methodology for such procedures is to force values into the code, referred to as stabbing, and extract output values from some intermediate place in the code process.
  • Regardless of the methodology or completeness of testing, the method discussed above only proves that the black box has the correct collection of elements, not that the elements are correctly connected. In other words, the verification process discussed above does not prove that the black box works properly end-to-end. It, therefore, does not prove that the black box, as a whole, will behave as intended.
  • Another shortcoming of this verification testing approach occurs everywhere that timing is involved, such as the verification that a timer expires as required. A simple verification at the desired expiration time does not preclude the black box from generating unexpected values at any or all of the intermediate, unverified times. Other issues of partial verification occur in the verification process of certain components or groups of components. These partial verification problems, which can be potentially very dangerous, can include: overlapping of data structures stored in memory but cannot be accessed; or “memory leaks”; incorrect connections between components, known as “stitching”; incorrect order of execution, such as loop-backs. None of these types of faults, and potentially others, would be detected.
  • Currently, verification has started to move from test cases that test component-by-component, or function-by-function to black box level verification. This level includes verification by test procedures that enter “real world” inputs into the black box which then generates real world outputs. The inputs are generated for each “run” of the program, or for each “frame”, to exactly mimicking the real application. In other words, the inputs are presented to the black box during the verification process exactly as they are presented in reality. Expected outputs are then produced for each run or frame, which are then compared to the collected actual outputs. This “continuous” method of verification is far superior to any other method, provided that the test procedures are able to exercise and verify each component and requirement of the black box.
  • However, the generation of such test procedures at the black box level is difficult for several reasons. Mainly, the variables used for inputs to a component, or block, may not be the same as the black box level real world inputs, and the outputs from the component, or block, may not be real world outputs from the black box. Therefore, the inputs to the element under test must be “demoted” to real world inputs, and the outputs from the element under test must be “promoted” to real world outputs. In other words, the verification process requires the test engineer to generate one test procedure for each targeted component, diagram, or block of components. The test procedure must be of a duration that addresses all timing issues, achieves the desired inputs using a combination of real world input values, and also generates real world outputs that are representative, in a detectable, unique way, of the targeted component outputs. The test procedure is complete when all the aspects of the targeted component are tested under the specified guidelines, such as modified condition/decision coverage, exhaustive, etc.
  • In the above environment, one way to generate independent expected outputs is to provide and run an alternative code in the black box. This is often referred as a “model,” but it could be just an alternative instantiation of the code, such as code independently produced by another team. Of course, it is desirable that the expected results are produced using a different compiler, a different hardware platform, and a different operating system than the black box.
  • Usually, one of the first problems encountered is reconcile differences between the expected results and the actual results. In a complex system, with thousand of components, this is a difficult task. A currently available method of performing reconciliation use the debugging features of two compilers in an integrated design environment (IDE), for example, compiling the model code side-by-side with the black box code. This method allows only “forward” debugging, meaning that both compilers must be stopped at the same point in the respective codes so that the user can look at values held by variables and data structures. The user then move to the next break point and again looks at values held by variables and data structures, and so on. The reconciliation process is difficult and may take very long time. Reconciliation is particularly long and difficult if the model is written using visual techniques, such as Simulink®, and/or if the input data to the black box cannot be provided faster than real time—it is normally provided much slower than real time. (Simulink® is a registered trademark of MathWorks, Inc., of 3 Apple Hill Drive, Natick, Mass. 01760.) The user may wait 10 minutes between break points, the point at which he may be able to investigate mismatching values, just to learn that the process must be started anew.
  • SUMMARY OF AN EMBODIMENT
  • In one embodiment, a layer of code is provided that “wraps around” the model code and at each execution of the code (at each frame of signal processing), saves the names of the variables explicitly (i.e. in ASCII format or any readable format with the name as it appears on the specifications, and not as a memory address) and saves also all the values assumed by that variable at each frame evaluation. Optionally, some other information will be saved, such as the type of variable, the time at which it was saved, etc., depending on the project. The variables for which the values are saved are all the variables in the system or a subset of them or even a superset (including special variables desirable for “setting the stage” of the test).
  • This innovative technique can be applied to any programming related to signal processing, i.e. to any program that receives a set of inputs and produces outputs at intervals, such as model-based verification as in DO 178B. Nevertheless, similar techniques could be expanded to any Integrated Development Environment (IDE).
  • While this technique is generally applicable to any computing environment, the technique is commercially enabled by the current availability of inexpensive memory for personal computers. As an example, consider a relatively complex signal processing system, with 5,000 variables. Consider also that a Test Procedure may have duration of 100 seconds and the signals are re-evaluated 100 times per second (10 millisecond frames). If each “value” saved uses “N” bytes, the required memory is 5,000×100×100×N=50×N Million Bytes. Assuming that N=16 Bytes (a reasonable assumption for saving one data point), this would be approximately 800 Megabytes of storage. Current offering of inexpensive Personal Computers commonly offer three to four times this amount, or more. The operating system (Windows XP or later), offers also nearly unlimited virtual memory on disk and is capable to address this amount of memory without problems.
  • The innovative technique described herein allows the user to select a point in time (for example using a slider or moving the mouse on a timeline) and inspect the values assumed by one or more selected variables (also clicked with mouse actions). Note that the user can go forward and reverse in the time selection on any value, and repeat at will, with immediate visualization of the results. The time required for this technology to display any value at any time is miniscule in comparison to alternative techniques. Of course, this technique requires the program (the Test Procedure or the “model”) to run entirely through once (without break points or debug settings) to completion, so that all the values can be saved.
  • In one possible implementation, the variables are shown in a convenient order (possibly in alphabetical order), and a small window allows a user to type any portion of a variable name the user intends to select. Matching variable names are then automatically highlighted and selected. Values for the selected variables can be automatically shown at the time selected by the mouse sliding back and forth on the canvas. If only one variable (or a few variables) are selected, there is enough room on the screen to show the values on a sliding window that shows, in the center, the value at the corresponding selected time, and also shows values for the same variable some frames before and some frames after the selected time.
  • In another implementation, the variables are shown in a window with a “scroll box”, and the values are shown for the desired time (frame) selection for the variables visible in the scroll box.
  • In yet another implementation, the selected (or all) variable(s) may be shown in graphical format. The arrangement of the values (color coded for positive/negative, Analog/Boolean, device related, etc.) is particularly important in model based verification, because “flag shaped” boxes can be displayed attached to points of interest on a diagram showing the desired functionality of the code. Since the flag-shaped boxes show the values of the signal at the spot indicated on the diagram at the time selected by the user moving the mouse on the canvas timeline, the debugging of a model-based becomes fast and easy.
  • A pseudo-code description of one embodiment of the process follows (it should be understood that the coding technique can vary widely).
  • The design engineer, test programmer or other user should perform the following initial steps:
      • Make a list of the procedures or function of interest that require execution at each step or frame.
      • For each procedure or function (or diagram), list the name of variables to the function as strings, in an array. This array should also contain the address (pointer) to where this variable is in memory. We will call this array “SimVar” This array may include other visual information, such as color to display, number of decimals or format with which to display the value, type of the variable, etc.
      • Depending on the desired effects of the Test Procedures, the user now populates the input values for all the Real World inputs. This is achieved by selecting appropriate signals and evaluating what input values are desired at each time in the input variables. Such values are stored in the arrays that hold the input and outputs, in time, for each variable (so far we are concerned only with inputs). We will call this array “DataSim”.
  • An automated program process is then run, for example, code which is “wrapped around” the Model Code The process is run in a way such that, for each SimVar at each DataSim input time, all outputs can be stored. The pseudocode for an example program process can be as follows:
  • { rTime is set as the beginning of the operation }
    { StepTime is the frame time }
    while rTime < (EndOfProcessingTime + StepTime/2) do
    begin
    Index := round (rTime / StepTime) ;
    { transfer values from DataSim to Simvar ONLY for INPUT
    variables }
     for i := low(SimVar) to High(SimVar) do
    SimVar[i].V{circumflex over ( )} := DataSim[i].TimedValues[Index].V ;
    { compute the output at this time }
    { execute all the desired model procedures here - this is one
    processing step only, for one frame }
    { then move the OUTPUT variables from SimVar to the
    DataSim timeline for the output data }
    rTime := rTime + StepTime ;
    end;
  • Conceptually, therefore, input signals are associated with input variable names, and then an input variable holds in a timeline all the desired input signal values for that variable.
  • At each computational frame of the Black Box, the collection of input values are transferred to memory using the pointers associated with the explicit variable names. Then, one computational event (frame) is evaluated and the Real World outputs are stored.
  • At the end, the values assumed by all the internal or Real World outputs are transferred to the appropriate variable's timelines using similar pointer associations between the list of tracked variables and memory locations.
  • As one example of the above, assume that a timeline is made of 100 seconds and 100 samples per second. The timeline for each variable thus contains 10,000 values. Then the above pseudo-code would be repeated 10,000 times to create a “SimRun”, but the execution time is not much more that executing the Black Box program itself, given that what is added is just moving data from one location in memory to another, for the tracked variables. The above process is executed ONCE and then all the data are ready to be displayed for any selected time (frame).
  • The showing portion of the program or “user interface” can then produce a “canvas” where a user can manipulate an input device such as a mouse or a touchscreen to select a time or times and variables to be viewed (perhaps adding a cross-hair), and data are then visualized (in any form) from the SimRun Timeline.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The patent or application file contains at least one drawing executed in color. Copies of this patent or patent application publication with color drawing(s) will be provided by the Office upon request and payment of the necessary fee.
  • The foregoing will be apparent from the following more particular description of example embodiments, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the embodiments.
  • FIG. 1 is a high level operations flow diagram.
  • FIG. 2 illustrates a main window of the user interface.
  • FIGS. 3-8 illustrate several example diagrams of signal processing components of a Black Box used as part of a Demo project.
  • FIGS. 9-14 illustrate various ways to verify certain diagrams.
  • FIG. 15 illustrates how to set IntelliPoints.
  • FIG. 16 is another verification view.
  • FIG. 17 illustrates verification of a timer.
  • FIG. 18 is a state diagram for timer verification.
  • FIGS. 19-21 are other timer verification diagrams.
  • DETAILED DESCRIPTION OF EMBODIMENTS
  • A description of example embodiments follows.
  • High Level Description of the Model-Based Verification Application
  • FIG. 1 is a high level operations flow diagram of an example embodiment of a Model-Based Verification Application 100.
  • to The Model-Based Verification Application 100 is made of several components.
  • Model Core: The Model Core 105 provides many of the features of the Model-Based Verification Application 100, such as generating input signal timelines using Intelligent Points, all graphical rendering and displaying of signals and corresponding signal processing components or blocks of connected components (also referred to hereafter as the “diagrams”), debugging capabilities, file name and file input/output (I/O) services.
  • UNITSCD: The UNITSCD (Specification Control Drawings) 110 is a code unit where all the information pertaining to the diagrams is stored. The information can include the devices, ASCII names of variables, the positions of flags, and constants on the diagram visual representations.
  • VARSANDBODIES: The VARSANDBODIES 115 enables the functionality of each diagram. It also enables the functionality of the complete Black Box under test by connecting together or “stitching” two or more of the diagrams that make up the Black Box. Typically, the VARSANDBODIES 115 is made up of calls to a library of components with standard behavior, or in some cases custom behavior. The library components can include, but are not limited to, Boolean logic gates, such as, OR gates, AND gates, and NOT gates, and other signal processing functions, such as delay timers, and various filters. The VARSANDBODIES 115 also provides all the variables of the Black Box in static memory.
  • This structure allows this same Model Core 105 to be re-used in different projects. New custom components can be added to the library of components as necessary. Using minimal additional resources, the custom components can be carried on as legacy elements in projects that do not use them.
  • The UNITSCD 110 and VARSANDBODIES 115 code units are typically new and unique for each project. Thus, they typically are developed for a specific project, and cannot be re-used in a different project. These code units can be considered to belong to a customer of the user. The VARSANDBODIES 115 needs to be compiled for performance, while the UNITSCD 110 is a database-like set of information.
  • Other (External) Model Components:
  • ALIAS Table: Alias Table 120 is a computer file, such as an Excel® file that contains information regarding names of variables used in the actual code, i.e., the code under test. (Excel is a registered trademark of Microsoft Corporation, One Microsoft Way, Redmond, Wash. 98052.) Such information can further include minimum and/or maximum limitations for values, granularity or decimation/digitalization properties, diagram stitching information, and other names in use. Information regarding other variable names in use is especially useful when there is redundancy, and/or inconsistency in the signal naming scheme among and between model code and actual code.
  • It should be understood by those of skill in the art that the mention of Excel® files throughout this document is due only to the convenience of using the Excel® format as a presentation layer, and not for any other features of Excel®. All specific file formats such as Excel, Visio, Simulink, Subversion, etc. referred to in this document can be in other formats, such as Comma Separated Values (.csv) or any other suitable form.
  • Diagram Bitmaps: Diagram Bitmaps 125 are a visual representation of the diagrams. The Diagram Bitmaps 125 can be a screen shot, or scan, of a diagram. While visual representations can be generated from the file that stores the diagram in native format, such as Visio®, Simulink®, or similar tool, it is preferred to use a bitmap file, because there are no possible errors in the interpretation of the native-mode files. In other words, what you see is what you get with bitmap files. (Visio is a registered trademark of Assistance Technique Et Etude De Materiels Electroniques Société Anonyme, France, Burospace Bâtiment 26 Route de Gizy; F-91570 Bievres, France; and Simulink is a registered trademark of MathWorks Inc., 3 Apple Hill Drive, Natick, Mass. 01760.) This preferred visual representation allows for an excellent independent interpretation and analysis of the diagram.
  • CMOD Files: CMOD Files 130 are computer files, such as Excel® files, that contain visual information, and environment or harness parameters about a specific test. The CMOD Files 130 contain only the “Intelligent Points” that allow the creation of complete test files in conjunction with the Model 101a/b.
  • Test Cases: The Test Cases 135 are a collection of computer files, such as Excel® files, which are related to a single diagram. In an example embodiment the columns represent all the input variables and output variables of the related diagram, and each row represents the inputs, and expected outputs, for each and every processing step. In other words, the Test Case 135 files contain all of the I/O variables, input values, and expected output values for each step of time along a timeline.
  • Test Procedures: Test Procedures 140 are a collection of files, such as Excel® files, which have columns representing Real World input values and output values. The input values contain all the initial condition values for variables. That is, Test Procedure 140 files contain all the Real World values that set the stage for the test, including the values for all the variables that have non-nominal values—even if they do not change during the test. The Real World output variables represented are a set of manually selected variables pertinent to a specific test. Each row represents input values and expected output values, for every time step. Each Test Procedure 140 is a companion to a Test Case 135, in the sense that the Test Procedure 140 will faithfully generate the Test Case 135 data for the related diagram, when the Real World input values traverse the diagram. In other words, when the Real World input values are completely processed according to a Test Procedure 140, the Test Case 135 data will be generated for the associated diagram.
  • Hardware (Rig): The Hardware (or Rig) 145 is the actual physical equipment against which the Model 101 is verified. Test Procedures 140 are submitted to the Hardware 145 to produce Actual Results, which are then fed back to the Model 101 and/or stored in record-keeping or version control systems 155, such as Subversion® or ClearCase®. (Subversion is a registered trademark of CollabNet, Inc., 8000 Marina Blvd., Suite 600, Brisbane, Calif. 94005; and ClearCase is a registered trademark of Atria Software, Inc., 24 Prime Park Way, Natick, Mass. 01760.)
  • Intelligent Points Setup and Manual Review Process:
  • The purpose of the Model-Based Verification Application 100 is to ascertain that each block in the Back Box, such as one or more selected components or diagrams, produces the intended functionality. The verification process is a complex function that depends on device type, signal type, required verification procedures, and several other parameters. Verification must sometimes also comply with applicable standards 170, such as DO178 as applied to flight code, and perhaps other custom requirements.
  • In a preferred example embodiment, each device can be verified by specifying a combination of Intelligent Points 175 (also referred to herein as “IntelliPoints”). An Intelligent Point is a command for a variable to assume a value, or a signal type, from one point in time until the point in time of the next Intelligent Point 175. In other words, an Intelligent Point 175 dictates the signal type for an input variable, and therefore input values, for a period of processing time along a time line. The simplest form of input variable signal is a linear interpolation between the two points, but other signal can be created in accordance with the selected attributes of the Intelligent Point 175.
  • While the number of Intelligent Points 175 in a particular Model 101 may vary depending on many considerations, normally a very small set of Intelligent Points 175 is sufficient for a particular verification. For example, a method for verification of a DelayOn device requires only four Intelligent Points 175 to generate the Boolean input values necessary to verify Persistency and Expiration tests. However, the Intelligent Points 175 must be carefully and appropriately set in time. For other variables more points may be required to promote the output signal to a visible Real World signal, using a promotion process.
  • The selecting or setting of Intelligent Points 175 can be achieved via a trial-and-error manual process, aided by the Model's 101 recalculation of all signals when a point is moved. Useful to selecting of Intelligent Points 175 is a real-time recalculation, which allows the user to graphically see the implications on all signals when an Intelligent Point 175 is modified in time, value or signal type, or another Intelligent Point 175 is added.
  • The combination of Intelligent Points 175 and real-time recalculation with graphical-aided feedback enables the Model-Based Verification Application 100 to verify the Black Box components. Without this combination, the Black Box verification of a complex system would exceed reasonable human resources.
  • User Interface:
  • FIG. 2 illustrates a user interface 200 for specifying various parts of the Model 101. The main window of the user interface 200 is organized in tabs 205. All options are preferably immediately visible with no hidden drop-down menus. All folder names 210 are always visible, and can be typed or browsed. Subsets of file names 215 can be selected by using a standard Windows mask. All parameters are saved in a local file for each PC, or user. All visible lists of files and produced tables can be saved in Excel® format for re-use.
  • Virtual Input Variable
  • The stitched Model 101 consumes all the Real World input variables and produces all the Real World output variables. However, the list of all the input variables can be impractical to maintain in some projects, therefore the Model 101 resorts to Intelligent Points 175 for Virtual Real World input variables. Here, for Virtual Real World input variables, it is intended as a variable that does not exist as a real world input variable, that may have a similar name to a Real World input variable, and has the purpose of setting a number of Real World input variables to the desired value or values, according to rules.
  • For example, the setting of a variable carried by a triple-redundant ARINC bus typically requires setting the value of 12 input variables; 3 values for each of the following: Data, Activity, Parity, and Sign/Status Matrix (SSM). A Virtual Real World input variable would set all 12 variables so that the internal variable selected after the redundancy process assumes the same value as the Virtual Real World input variable.
  • In another example, an input variable can assume a value in degrees inside the Black Box, or even inside a particular diagram, but has a real world input variable value in radians, or Sines and Cosines, the Virtual Real World input variable is set in degrees, and the Model 101 adjusts the input values to Sines and Cosines accordingly.
  • The Virtual Variable can be set to any value, but the Model 101 limits the Real World input values according to the specified minimum and maximum values in the Alias table 120 (shown in FIG. 1) and only produces values that match the actual granularity of the input values, i.e., the digitized or decimated values, so that the variables internal to the Black Box can only assume values that can be carried through the physical hardware. This is useful so that model-computed expected results can exactly match Black-Box computed actual results.
  • Ranges for Variables
  • In the real world, physical hardware, variable values are carried to the Black Box model via communications channels or buses. Usually, a bus or channel has a width in bits.
  • For example, if the variable is generated by a 10-bit analog-to-digital converter (A/D), the bus may also have a 10-bit width. Assuming, as an example, a 10-bit A/D is connected to a sensor that measures Vertical Speed Accelerations (VSA) in gravitational-force (Gs). Further assuming that the aircraft in which the VSA is installed is designed to operate between −3 and +7 Gs, and that the device will disintegrate if the acceleration exceeds the range between −6 and +14 Gs. The sensor is capable of providing data values between −20.48 and +20.44 Gs.
  • The example assumed will be able to accommodate 1024 discrete values. Further assuming that one bit is used for the sign, and that −20.48 G would correspond to −512 and +20.44 G would correspond to 511. It is useful to introduce a scale to convert from the raw input data signal to a more meaningful, and floating point, value. In this case, the scale would be 1/25. (Range of values±Number of discrete values for the range=(20.44−(−20.84))/(1024−1)=1/25.) This would also implicitly dictate that the signal is received in minimum increments (granules, decimation, or digitization units) of 0.04 Gs.
  • In the above example, the Alias table 120 would carry the information about range and granularity for this variable. The Model 101 would use the Alias table 120 to create input values only in accordance with the range and granularity. Although the variable input can assume values from −20.48 to +20.44 Gs, in 0.04 increments, the values outside of the range between −6 and +14 Gs are meaningless, because, in the real world the VSA sensor would be destroyed. It would useful that a project have a limiting layer of code that ensures that all input variable values are meaningful operational values.
  • Demo Project
  • In the following discussion of several drawings, it is assumed that the specifications are for a Demo project.
  • FIG. 3 is an example of an analog limiting and combining diagram 301 a, for which the input variable ranges are specified, contained within the Black Box. The tabs 370 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. For example, VAR_S_A 302 can range from a MAX_SA 303 value of +21.0 down to a MIN_SA 305 of −8.0. Similarly, VAR_S_B 312 ranges from a MAX_SB 313 value of +7.0 down to a MIN_SB 315 of −7.0 and VAR_S_C ranges from a MAX_SC 323 value of +10.0 down to a MIN_SC 325 of −10.0. The limiters 350 produce the Real World output variables, VAR_S_A_LIM 307, VAR_S_B_LIM 317, and VAR_S_C_LIM 327. The combiner 360 use Real World output variables VAR_S_A_LIM 307, VAR_S_B_LIM 317, and VAR_S_C_LIM 327 to produce VARS_S_AB 319 and VAR_S_AC 329. The input variable values ranges, MAX_SA 303, MIN_SA 305, MAX_SB 313, MIN_SB 315, MAX_SC 323, and MIN_SC 325 are shown in green. Window pane 301 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as input/internal/output (I/N/O), visibility, decimals, color, line width (LW), scale/bias, actual value, and variable name, for the diagram 301 a.
  • FIG. 4 illustrates another diagram 401 a inside the Black Box containing different types of components, such as DelayOn 405, Boolean gates 406, 407, and a decision making comparator 408. The tabs 470 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. The flag-shaped rectangles, with a numeric or Boolean value inside, or flags 402, are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams. The components DelayOn 405, Boolean gates 406, 407, and decision making comparator 408, operate in accordance with their respective function and connections, or stitching, on the values associated with VAR_B_Z 411, VAR_B_Y 412, VAR_B_X 413, VAR_B_W 419, VAR_S_U 415, and VAR_S_T 416 to produce output variables VAR_B_ZOR 421, VAR_B_WXY 422, and VAR_B_TU 423. Window pane 401 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 401 a.
  • FIG. 5 illustrates yet another example diagram 501 a containing a Differentiator (S) 551, Integrator (1/S) 552, Limited Integrator 553 and a couple of First-Order filter components 554. The tabs 570 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. The flags 502, are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams. The components Differentiator (S) 551, Integrator (1/S) 552, Limited Integrator 553 and couple of First-Order filter components 554 operate in accordance with their respective functions and connections on the values associated with input variables VAR_S_A_LIM 307, VAR_S_B_LIM 317, and VAR_S_C_LIM 327 to produce output variables VAR_S_A_DIFF 521, VAR_S_B_INTEG 522, VAR_S_B_INTLIM 523, VAR_S_C_FILT 524 and VAR_S_C_FOFILT 525. Window pane 501 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 501 a.
  • FIG. 6 exemplifies yet another example diagram 601 a that has four different Second-Order filters 650. The tabs 670 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. The six constants 653, the numbers shown in green, define the response characteristics of each Second-Order filter 450. The parameters of the Second-Order filters 450 are shown in the S-domain, but Z-domain parameters can also be used. The flags 602, are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams. The Second-Order filter components 650 operate in accordance with their respective functions, including their respective response characteristics, and their connections on the values associated with input variable VAR_S_C_LIM 327 to produce output variables VAR_S_C_HPFILT 621, VAR_S_C BPFILT 622, VAR_S_C_BSFILT 623, and VAR_S_C_SOFILT 624. Window pane 601 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 601 a.
  • FIG. 7 shows another example diagram 701 a a special type of Second-Order filter, a Notch Filter 750. The tabs 770 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. The six constants 753, the numbers shown in green, define the response characteristics of the Notch filter 750. The parameters of the Notch filter 750 are shown in the S-domain, but Z-domain parameters can also be used. The Notch filter component 750 operates in accordance with its respective function, that is filtering according to its response characteristics, and connections, on the values associated with input variable VAR_S_C_LIM 327 to produce output variables VAR_S_C_NOTCH 721. Window pane 701 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 701 a.
  • FIG. 8 illustrates a diagram 801 a in which analog and Boolean (digital) variables are processed for presentation to a Real World output layer. The purpose of this diagram is to exercise the stitching between diagrams and components and the promotion process of moving virtual variables to the Real World. The tabs 870 indicate different diagrams, or sets of interconnected signal processing components, contained within the Black Box. The flags 802, are set up by the Model 101 to show the value of variables and other components at a given time, and are not part of the specifications or diagrams. The components, switches 850 and mixer 851, operate in accordance with their respective functions and connections on the values associated with input variables VAR_S_A_DIFF 521, VAR_B_ZOR 421, VARS_S_B_INTEG 522, VAR_S_B_INTLIM 523, VAR_S_C_FILT 524, VAR_B_WXY 422, VAR_S_C_FILT 524 VAR_S_C_FOFILT 525 and VAR_B_TU 423 to produce output variables VAR_S_AB_OUT 821, VAR_S_BC_OUT 822, and VAR_S_C_OUT 823. Window pane 801 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 801 a.
  • FIG. 9 is an example of a timeline plot of signals used for verification of the diagram with limiters 301 a (shown in FIG. 3). The canvas 901 a depicts a 30 second timeline of signals 910, 920, and 930. The window pane 901 b on the left contains a list of all variable inputs (here, all Virtual) and all variables output to the Real World. The three waveforms of signals 910, 920, and 930 each have an amplitude that exceeds the limits of the values for the input variables corresponding to the respective limiters 350 (shown in FIG. 3). Therefore, the signals 910, 920, and 930 are useful to verify, at least partially, the performance of the limiters 350.
  • FIG. 10 is another diagram illustrating an alternate example approach to verification of the diagram 301 a with limiters (FIG. 3). Canvas 1001 a depicts a 30 second timeline of signals 1010, 1020, and 1030. Here, the three waveforms, signals 1010, 1020, and 1030, are obtained suing a few IntelliPoints 1050. A single IntelliPoint 1050 defines each of the periodic sinusoidal waveforms 1010 (colored purple) and 1030 (red) by setting their respective frequencies in Hertz, and amplitudes. The waveform signal 1020 (green) is generated by linear interpolation between the adjacent IntelliPoints 1050 in a set of four IntelliPoints 1050.
  • FIG. 11 illustrates an example verification of the limiter diagram 301 a (FIG. 3) in another way. The values for the input variables and output variables are plotted as a function of time on the canvas 1101 a. Here, in window pane 110 ab, the user can inspect the variables local to the diagram 301 a at the same time as he or she sets the Real World input values. The effect of the limiters 350 is obvious from the chopping of peaks and troughs shown in the output signals 1114, 1115, 1116, 1117, and 1118 generated from the sinusoidal waveform input signals 1111, 1112, and 1113. Dragging an IntelliPoint to reposition it along the canvas has an immediate effect on both windows, allowing the user to gauge the verification effort.
  • FIG. 12 illustrates an example verification of the limiter diagram 301 a (FIG. 3). Canvas 1201 a depicts a 30 second timeline of signals 1210, 1220, and 1230. Here, the three waveforms, signals 1210, 1220, and 1230, are obtained suing a few IntelliPoints 1050. A single IntelliPoint 1250 defines each of the periodic sinusoidal waveforms 1210 (colored purple) and 1230 (red) by setting their respective frequencies in Hertz, and amplitudes. The waveform signal 1220 (green) is generated by linear interpolation between the adjacent IntelliPoints 1250 in a set of four IntelliPoints 1050. In FIG. 12 linearly interpolation between each of four IntelliPoints 1250 (green) shows that the signal is sufficient for the verification of one of the limiters 350 (FIG. 3). The other limiters 350 are verified by waveform signals created by setting one single Intelligent Point for each signal, where each generated a sinusoidal signal has amplitude exceeding each respective limiter's threshold.
  • FIG. 13 depicts another example diagram 1301 a, which show the values of all the variables at that time in the flags 1302. The flags 1302, containing variable values at the specified time step, are over-imposed to the bitmap of the diagram 1301 a. In a preferred embodiment, example diagram 1300 is displayed at the same time as the verification display 1200 (FIG. 12). Other features of the figure have been previously described.
  • FIG. 12 in combination with FIG. 13 illustrates a useful feature in canvas 1201 a (FIG. 12) is that the crosshair can be moved back and forth in time along the timeline, and the variables values can be immediately shown to the user in the flags 1302 (FIG. 13) without re-computing. Re-computing is unnecessary because all variable values, at all time points within the canvas, have already been computed and saved. Thus, when the user selects a different point on the time line, such as by moving the cross-hair, the variable values at the newly selected time are determined simply by looking them up in an array, the DataSim table, and displayed in the flags. Re-computation occurs only when an IntelliPoint is changed.
  • Therefore, the model therefore enables the selective visualization of output variables, allowing a user to immediately determine if a Real World output is a viable function, such as a linear transfer function, or the best possible approximation, of the selected diagram output.
  • FIG. 14 illustrates another example embodiment of a step in a verification method. In order to verify end-to-end operation of a Black Box, it is useful to select a Real World output variable that unequivocally represents the diagram output variable. This can be achieved through a process called promotion, in which a signal is promoted towards the output. It is useful to unequivocally represented a signal that is the output variable of a diagram, but is an intermediate variable, i.e., a non-Real World output of the Black Box. This can be accomplished by navigating to diagrams downstream of the diagram under test (i.e., signal processing functions that occur later in the Model 101 process) and selecting suitable variables that represent the original signal as the output. Here, the diagram under test is diagram 301 a (shown in FIG. 3), and an intermediate variable is VAR_S_AB_OUT 1410. Canvas 1401 a depicts a 30 second timeline of signals 1010, 1020, and 1030. Window pane 1402 displays a data for intermediate variable is VAR_S_AB_OUT 1410, including values and time increments for each processing frame number and the frame number.
  • FIG. 15 illustrates a preferred graphical user interface (GUI) 1501 for selecting or setting IntelliPoints. The choice of the parameters for the IntelliPoints can be simple and intuitive. The following commands are preferably used in a graphical view of input variable values as a function of time, such as illustrated in FIG. 14: a left-click of a mouse allows a user to drag-and-drop the IntelliPoint to a new location; a center-click deletes the IntelliPoint; and, a right-click opens a window, such as for the GUI 1501, where the user can set a variety of parameters. As shown in GUI 1501, a variety of attributes can be selected to create functions for input variable values, such as normal (i.e., linear interpolation) 1510, frequency 1511, pulses 1512, square wave 1513, saw wave 1514, hold value (i.e., set to a constant) 1515, and frequency increment 1516. Depending upon the function selected, such as frequency increment 1516, for example, certain other IntelliPoint parameters will become available to the user.
  • An example embodiment of a disclosed method can ultimately result in a CMOD file 130 (FIG. 1). FIG. 16 illustrates the CMOD files contents 1600 for the verification of a relatively complex diagram. While the CMOD file is shown in Excel®, the user never has to manually operate within Excel® program. The CMOD file 130 and 1600 represents a complete Test Procedure.
  • Verification of a Diagram with Timer on Boolean Logic
  • FIG. 17 illustrates a typical diagram 1701 a for timer verification containing a set of logical rules. It should be understood that such rules can vary depending upon project requirements. In this case, the Boolean logic is normally tested using Modified Condition/Decision Coverage (MCDC). Other aspects and features of the figure have been previously described in discussions regarding FIG. 4, the difference being that in FIG. 17 the variable values of the diagram 1701 a are shown for time 7.76 seconds.
  • FIG. 18 show a state event diagram 1800 for timer logic, such as that illustrated in 1701 a (FIG. 17). In this case, according to the State-Event diagram 1800, the requirements mandate the timer, having Boolean input values and output values, to be verified for persistency and expiration. The State-Event diagram 1800 illustrates that only four Intelligent Points, when properly allocated in time along the timeline, satisfy the requirement.
  • FIG. 19 illustrates an example method of verifying the timer on Boolean logic diagram 1701 a (FIG. 17). The setting of four IntelliPoints 1950, between 4 seconds and 14 seconds on the canvas 1901 a, is sufficient to verify the timer. Window pane 1901 b illustrates a listing of the input variables and output variables and the attributes corresponding to each, such as I/N/O, visibility, decimals, color, LW, scale/bias, actual value, and variable name, for the diagram 1901 a.
  • FIG. 20 illustrates an example verification method of the diagram 1701 a (FIG. 17) in another way. The canvas 2001 a in window 2000 shows the variables related to the diagram under test only, such as VAR_BZ 2010, VAR_BY 2020, VAR_BX 2030, VAR_BW 2040, VxB1 2050, VAR_B_ZOR 2060, VAR_B_WXY 2070, and VAR_B_TU 2080.
  • FIG. 21 illustrates verification of the diagram 700 with Notch Filter (FIG. 7). The notch filter is verified by appropriately selecting a few IntelliPoints. One IntelliPoint sets a variable-frequency waveform 2110, another IntelliPoint sets a square wave (impulse response), and another IntelliPoint sets a frequency 2115 tuned to the expected “notch.” The amplitude of the response characterizes the filter parameters. The Test Case results in an Excel® file with 1500 rows (30 frames at 20 millisecond per frame).
  • Advantages of an Embodiment
  • In an example embodiment, the Test Cases generated using appropriately selected IntelliPoint verify all the relevant and necessary variables at all signal processing frames. The Test Procedures compare expected results, those produces by the Model, and actual results, those produced by the Black Box, for all the variables at each and every frame, leaving no uncertainties regarding random, unexpected variable values or wrong stitching between diagrams.
  • The IntelliPoints are similar to fractals in that IntelliPoints expand to a lengthy and complex Test Case and Test Procedure files. This expansion process is relatively simple and the Test Cases and Test Procedures are automatically generated by the Model. While the Test Case and Test Procedure files are lengthy and complex, at the same time, the IntelliPoints are humanly understandable and settable, with the aid of the backward and forward timeline traversal debugging and visualization features of the Model.
  • An example embodiment of the method has been proven successful in a project with 200 complex diagrams and 6,000 variables, while still providing reasonably approximate real time feedback when moving IntelliPoints. In the test case, the 500 CMOD files, having an average of 20 IntelliPoints each, produced four giga bytes (4 GB) of Excel® Test Cases and Test Procedures in about 6 hours of batch processing on a medium-powered PC. The complete verification process produces only IntelliPoints that verify the desired specifications for all components. With this method, each Intelligent Point only requires a few minutes of user attention. This is particularly useful to save time in the event that the requirements change; the user needs only to add or modify a few Intelligent Points, after which the system can re-compute all expected results for all diagrams.
  • The batch process that re-computes output variable values at all times is particularly useful because a change in requirements, or a change in a diagram, can significantly alter the expected results, and is very difficult to predict. Then, the batch process may produce then correct verification, which perhaps is incomplete. The verification of a component is complete only when the component is fully exercised according to specification. However, an incomplete verification is still useful if the expected results match the actual results. The completion of the verification may be achieved in steps, for example, by adding Intelligent Points, to the existing Test Cases and Test Procedures.
  • The above described forward and reverse timeline traversal debugging technique is more than simply moving a mouse back and forth on a timeline. It is a complex balance of programming resources allocation. It provides the user with the perception that all the variables in all the diagrams are immediately recalculated for any change to the Intelligent Points and other parameters, and that all the values are immediately available at the time frame where the mouse is positioned on the timeline. This perception of real-time availability is useful to enable the interactive interface allowing the user to easily and quickly set IntelliPoints for verification. Test Case is manually generated, and the generation process is aided by the real-time feedback of the expected results, immediately available to the user to explore for each device and each variable at any time interval along the timeline.
  • Consider the typical software code to be verified, such as a control law for avionics, or medical applications, while appearing very complex, it is usually designed to run at a duty cycle of 40 percent or less on an inexpensive microchip, which perform digital signal processing in computational “frames” of a few milliseconds. Rarely there are complex, non linear, mathematical algorithms needed. And if such complex algorithms are needed, they are highly optimized. Furthermore, rarely does a single test case required more than a 30 second timeline to prove that one aspect of the design is verified. However, many test cases may be required—normally a few per diagram. In other words, if the model of the program under test, produced by an independent interpretation of the requirements diagrams, is compiled on a relatively fast PC in “C” or Pascal, with virtually no memory constraints, the Test Case that would take microchip CPU time of 12 seconds (40% of 30 seconds), takes only a few seconds to run on the PC. This is an acceptable real time-response for the test engineer that changes a meaningful parameter—but it is not acceptable for looking at the changing values of variables when a mouse is moved on the timeline. When the engineer explores the possibilities of changing signals, the response time of the program must be much quicker. The above described forward and reverse timeline traversal debugging technique stores all the values for a complete timeline run within a few seconds, but allows the user to select a time, for example by using mouse movement or using arrow keys, and immediately—within milliseconds—see the values for all the variables.
  • The manual generation of Test Cases, aided through the use of timeline views of the signals, is not possible if the model program is written in an interpretative or semi-interpretative language. Experience with a large project provided that an environment such as PYTHON® has a greater than 10× response time, and SIMULINK® has a greater than 100× response time compared to a streamlined, compiled PASCAL rendition in which all variables are in static memory. (PYTHON is a registered trademark of Python Software Foundation Corporation, P.O. Box 37 Wolfeboro Falls, N.H. 03896-0037.)
  • After establishing that the Model code runs in a few seconds or less, two other features are useful in providing the perception of immediacy in displaying of data to the Test Case designer.
  • The first feature is the fact that the program tracks which diagram the user is viewing. The user can only look at one diagram at a time. Thus, when the user changes a diagram tab, a two second time for recalculation is acceptable. When the program tracks the diagram under test and the information associated with it, such as the position the flags on the diagram, the Model Core only needs to lift the values of the variables the user can see from static memory, at end of each computational frame. This can be done without disturbing the model code execution or adding cycles to it. The data is quickly accessed and copied from the variable's values, at each computational frame, are stored sequentially in memory, for immediate access, with access via frame number. This allows the corresponding values to be immediately displayed when the engineer selects any time corresponding to a computational frame. While it is true that all the data could be saved at each frame, it would require many gigabytes of memory for a large project, and the program would be slow for a variety of other reasons, such as memory paging.
  • Therefore, all the data related to all the I/O variables that the user can actually “see” on the timeline, and only those I/O variables, appropriately organized in meaningful groups, are stored in a memory array for each frame of execution along the timeline. The data related to the I/O variables that the user can see may include either the flag over the variable name in the diagram bitmap or the variable plotted with appropriate bias and colors.
  • After the data has been stored, when the user moves the mouse on the timeline plot, the model core only displays all the variables that the user can see on the diagram under being viewed. Since this process typically takes a very short time for a reasonable diagram, for example, less than 100 milliseconds after the mouse settles, the user perceives that the program responds immediately.
  • Also useful is the fact that the user does not have to type the variable names; the values of all the variables that can be seen are immediately reported. The user needs only to select the time (i.e. processing frame) with a single mouse motion—for any frame in the timeline—moving the cross-hair on the canvas.
  • Sometimes diagrams pre-consume variables that are produced later during the computational chain. In other words, a variable assumes two different values during a single computational frame, such as when an output signal is fed back to some input. In an example embodiment, pre-consumption is solved by storing the value of the intermediate, non-Real World I/O variables at the time when the diagram under test is executed, in the order of execution chain, and not at the end of the computational frame. This feature can also be bypassed, if the need arises.
  • The teachings of all patents, published applications and references cited herein are incorporated by reference in their entirety.
  • While this invention has been particularly shown and described with references to example embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the scope of the invention encompassed by the appended claims.

Claims (5)

1. A method of debugging a model-based signal processing program comprising:
selecting a set of output variables;
selecting parameters of a time line, including at least a start time, a time increment, and an end time;
for each increment of time between the start time and end time, determining values for the selected set of variables at each such increment of the time line; and
saving the values so determined;
at a later time,
retrieving at least a portion of the saved values;
displaying a graphical representation of the values of the variables over at least a portion of the time line, along with at least one numerical representation of at least one variable at a selected time; and
providing a user-manipulable element of the graphical representation that is used to specify the selected time, and such that the user-manipulable element can be visually moved backward and forward along the graphical representation,
thus providing immediate visualization of the numerical representation of the variables at any given time after the step of saving.
2. The method of claim 1 wherein the steps of selecting the set of variables and/or selecting the parameters of the time line are performed a second time, without re-performing the steps of determining values for the selected set of variables.
3. A method of visualization of variable data values on a diagram of a signal processing system, whereby a user can immediately visualize the variable data values at any desired time along a time line, thus allowing the understanding of the operation of the diagram at a pace set by a user, with an option to move forward or reverse along the time line.
4. The method of claim 1 further wherein:
the steps of determining, saving, and retrieving the saved values are performed for all variables at all possible computational steps, and
a cost of storage, simplicity and/or safety of storage techniques and/or ease of retrieval for display purposes are determined at selected times on the time line.
5. A method of verifying the operation of a software program comprising:
developing a model of the program;
capturing variable data at all increments along a selected time line, such that a visual data trace of the variable data can be represented as discrete samples in time during the entire execution of the model of the program, thus allowing the captured variable data to be inspected in both forward and reverse time.
US13/302,546 2010-11-22 2011-11-22 Model Based Verification Using Forward and Reverse Traversal of Variable Time Line Abandoned US20120192158A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/302,546 US20120192158A1 (en) 2010-11-22 2011-11-22 Model Based Verification Using Forward and Reverse Traversal of Variable Time Line

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US41615210P 2010-11-22 2010-11-22
US41615310P 2010-11-22 2010-11-22
US45841010P 2010-11-23 2010-11-23
US45840610P 2010-11-23 2010-11-23
US201161481973P 2011-05-03 2011-05-03
US13/302,546 US20120192158A1 (en) 2010-11-22 2011-11-22 Model Based Verification Using Forward and Reverse Traversal of Variable Time Line

Publications (1)

Publication Number Publication Date
US20120192158A1 true US20120192158A1 (en) 2012-07-26

Family

ID=46544822

Family Applications (3)

Application Number Title Priority Date Filing Date
US13/302,537 Abandoned US20120192013A1 (en) 2010-11-22 2011-11-22 Verification of Signal Processing Using Intelligent Points
US13/302,632 Expired - Fee Related US9020796B2 (en) 2010-11-22 2011-11-22 Model based verification using intelligent connectors
US13/302,546 Abandoned US20120192158A1 (en) 2010-11-22 2011-11-22 Model Based Verification Using Forward and Reverse Traversal of Variable Time Line

Family Applications Before (2)

Application Number Title Priority Date Filing Date
US13/302,537 Abandoned US20120192013A1 (en) 2010-11-22 2011-11-22 Verification of Signal Processing Using Intelligent Points
US13/302,632 Expired - Fee Related US9020796B2 (en) 2010-11-22 2011-11-22 Model based verification using intelligent connectors

Country Status (1)

Country Link
US (3) US20120192013A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111060325A (en) * 2019-12-13 2020-04-24 斑马网络技术有限公司 Test scene construction method and device, electronic equipment and storage medium
CN111459369A (en) * 2020-04-13 2020-07-28 深圳康佳电子科技有限公司 Interface element screening method, intelligent terminal and storage medium
US10747921B2 (en) 2016-01-05 2020-08-18 Cyient, Inc. Software tool for simulating operation of hardware and software systems

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10120785B2 (en) 2016-10-21 2018-11-06 Rosemount Aerospace Inc. Automatic generation of data coupling and control coupling test conditions
CN108647146B (en) * 2018-05-11 2021-06-08 北京信息科技大学 Test case generation method for judging combination coverage based on correction condition
US11010285B2 (en) 2019-01-24 2021-05-18 International Business Machines Corporation Fault detection and localization to generate failing test cases using combinatorial test design techniques
US11106567B2 (en) 2019-01-24 2021-08-31 International Business Machines Corporation Combinatoric set completion through unique test case generation
US11010282B2 (en) 2019-01-24 2021-05-18 International Business Machines Corporation Fault detection and localization using combinatorial test design techniques while adhering to architectural restrictions
US11099975B2 (en) 2019-01-24 2021-08-24 International Business Machines Corporation Test space analysis across multiple combinatoric models
US11263116B2 (en) * 2019-01-24 2022-03-01 International Business Machines Corporation Champion test case generation
US10970197B2 (en) 2019-06-13 2021-04-06 International Business Machines Corporation Breakpoint value-based version control
US10970195B2 (en) 2019-06-13 2021-04-06 International Business Machines Corporation Reduction of test infrastructure
US10990510B2 (en) 2019-06-13 2021-04-27 International Business Machines Corporation Associating attribute seeds of regression test cases with breakpoint value-based fingerprints
US11422924B2 (en) 2019-06-13 2022-08-23 International Business Machines Corporation Customizable test set selection using code flow trees
US11232020B2 (en) 2019-06-13 2022-01-25 International Business Machines Corporation Fault detection using breakpoint value-based fingerprints of failing regression test cases
US10963366B2 (en) 2019-06-13 2021-03-30 International Business Machines Corporation Regression test fingerprints based on breakpoint values
CN111337779A (en) * 2020-03-26 2020-06-26 上海精密计量测试研究所 Component on-orbit flight evaluation verification method

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3142820A (en) * 1960-01-20 1964-07-28 Scam Instr Corp Variable monitoring and recording system
US6286017B1 (en) * 1995-02-22 2001-09-04 EGILSSON áGUST SVERRIR Graphical environment for managing and developing applications
US20030061541A1 (en) * 1999-06-03 2003-03-27 Kaler Christopher G. Method and apparatus for analyzing performance of data processing system
US6795963B1 (en) * 1999-11-12 2004-09-21 International Business Machines Corporation Method and system for optimizing systems with enhanced debugging information
US20050228630A1 (en) * 1998-08-31 2005-10-13 Tseng Ping-Sheng VCD-on-demand system and method
US20110016358A1 (en) * 2007-09-14 2011-01-20 Airbus Operations (Societe Par Actions Simplifiee) Method for debugging operational software of a system onboard an aircraft and device for implementing the same
US8255875B2 (en) * 2008-09-30 2012-08-28 Rockwell Automation Technologies, Inc. Application builder for industrial automation

Family Cites Families (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5815654A (en) 1996-05-20 1998-09-29 Chrysler Corporation Method for determining software reliability
US5953009A (en) * 1997-05-27 1999-09-14 Hewlett-Packard Company Graphical system and method for invoking measurements in a signal measurement system
US6054984A (en) * 1997-05-27 2000-04-25 Hewlett-Packard Company System and method for graphically manipulating display elements in a signal measurement system
US6141630A (en) 1997-08-07 2000-10-31 Verisity Design, Inc. System and method for automated design verification
US6320577B1 (en) * 1998-11-03 2001-11-20 Agilent Technologies, Inc. System and method for graphically annotating a waveform display in a signal-measurement system
US6937965B1 (en) 1999-12-17 2005-08-30 International Business Machines Corporation Statistical guardband methodology
US7146605B2 (en) 2001-01-15 2006-12-05 International Business Machines Corporation Automatic abstraction of software source
US7188091B2 (en) 2001-03-21 2007-03-06 Resolutionebs, Inc. Rule processing system
US6965887B2 (en) 2001-03-21 2005-11-15 Resolutionebs, Inc. Rule processing methods for automating a decision and assessing satisfiability of rule-based decision diagrams
US20030154063A1 (en) * 2002-02-08 2003-08-14 Martin Lu Active path extraction for HDL code
US6885212B2 (en) * 2002-06-25 2005-04-26 Fujitsu Limited Semiconductor device and test method for the same
US7203631B2 (en) 2002-09-09 2007-04-10 Intel Corporation System and method to analyze VLSI designs
JP4247517B2 (en) * 2002-11-15 2009-04-02 富士通テン株式会社 Waveform editing program, waveform editing apparatus, and waveform editing method
US7913232B2 (en) 2003-02-21 2011-03-22 The Math Works, Inc. Certifying software for safety-critical systems
US7694276B2 (en) 2003-02-28 2010-04-06 Microsoft Corporation Contracts and futures in an asynchronous programming language
US7827526B2 (en) * 2003-06-13 2010-11-02 Analog Devices, Inc. Stacking and repeating graphical controls
EP1665034B1 (en) * 2003-08-13 2017-03-22 National Instruments Corporation Creating a graphical user interface for selected parameters of a graphical program
US7496480B2 (en) * 2003-08-15 2009-02-24 National Instruments Corporation Sweep manager for signal analysis
US20070213940A1 (en) * 2003-09-04 2007-09-13 Brent Rardin Analysis Device Operational Methods and Analysis Device Programming Methods
US7580037B1 (en) * 2003-09-05 2009-08-25 Altera Corporation Techniques for graphical analysis and manipulation of circuit timing requirements
US7552102B2 (en) 2003-09-29 2009-06-23 Huelsman David L Rule processing method, apparatus, and computer-readable medium to provide improved selection advice
US7003420B2 (en) 2003-10-31 2006-02-21 International Business Machines Corporation Late binding of variables during test case generation for hardware and software design verification
US20050114838A1 (en) 2003-11-26 2005-05-26 Stobie Keith B. Dynamically tunable software test verification
JP2005164338A (en) * 2003-12-01 2005-06-23 Fujitsu Ten Ltd Inspection device for control unit, pattern signal generation device and inspection program generation device
ATE526628T1 (en) 2004-01-22 2011-10-15 Nec Lab America Inc SYSTEM AND METHOD FOR MODELING, ABSTRACTING AND ANALYZING SOFTWARE
US7278056B2 (en) 2004-06-09 2007-10-02 International Business Machines Corporation Methods, systems, and media for management of functional verification
US7734559B2 (en) 2004-09-28 2010-06-08 Huelsman David L Rule processing method and apparatus providing exclude cover removal to simplify selection and/or conflict advice
US7779382B2 (en) 2004-12-10 2010-08-17 Microsoft Corporation Model checking with bounded context switches
US7793269B2 (en) 2005-02-15 2010-09-07 Ebay Inc. Parallel software testing based on a normalized configuration
JP4625978B2 (en) * 2005-04-22 2011-02-02 テクトロニクス・インターナショナル・セールス・ゲーエムベーハー Signal generator and parameter editing screen layer display method
US7930659B2 (en) 2005-06-03 2011-04-19 Nec Laboratories America, Inc. Software verification
US7797687B2 (en) 2005-08-04 2010-09-14 Microsoft Corporation Parameterized unit tests with behavioral purity axioms
US7757121B1 (en) 2006-04-21 2010-07-13 Cydone Solutions Inc. Requirement driven interoperability/compliance testing systems and methods
US20080255681A1 (en) * 2007-04-10 2008-10-16 Cindy Alsup Scott Methods and apparatus to manage process plant alarms
US7725772B2 (en) 2007-07-18 2010-05-25 Novell, Inc. Generic template to autogenerate reports for software target testing
US20090077532A1 (en) 2007-09-13 2009-03-19 Universities Space Research Association Automated annotation inference for safety certification of automatically generated code
US8020137B2 (en) * 2007-12-17 2011-09-13 International Business Machines Corporation Structure for an on-demand power supply current modification system for an integrated circuit
US20090165125A1 (en) * 2007-12-19 2009-06-25 Research In Motion Limited System and method for controlling user access to a computing device
US20090199160A1 (en) * 2008-01-31 2009-08-06 Yahoo! Inc. Centralized system for analyzing software performance metrics
US8423879B2 (en) 2008-05-14 2013-04-16 Honeywell International Inc. Method and apparatus for test generation from hybrid diagrams with combined data flow and statechart notation
US7679391B2 (en) * 2008-07-11 2010-03-16 Advantest Corporation Test equipment and semiconductor device
DE112009002304T5 (en) * 2008-09-29 2012-01-19 Fisher-Rosemount Systems, Inc. Efficient design and configuration of elements in a process control system
US8374094B2 (en) * 2008-12-11 2013-02-12 Fisher-Rosemount Systems, Inc Methods and systems to verify a communication path between a field device and a process controller in a process control system
US8612938B2 (en) 2009-01-05 2013-12-17 Tata Consultancy Services Limited System and method for automatic generation of test data to satisfy modified condition decision coverage
US8176454B2 (en) * 2009-08-28 2012-05-08 Empire Technology Development Llc Non-invasive timing characterization of integrated circuits using sensitizable signal paths and sparse equations
US8396420B2 (en) * 2009-12-30 2013-03-12 Ubidyne, Inc. Active antenna system for a mobile communications network as well as a method for relaying a plurality of radio signals through the active antenna system
EP2598989B1 (en) 2010-07-30 2020-03-11 National Instruments Corporation Developing programs in a graphical specification and constraint language
US9645715B1 (en) * 2014-01-10 2017-05-09 Cadence Design Systems, Inc. System, method, and computer program product for electronic design visualization

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3142820A (en) * 1960-01-20 1964-07-28 Scam Instr Corp Variable monitoring and recording system
US6286017B1 (en) * 1995-02-22 2001-09-04 EGILSSON áGUST SVERRIR Graphical environment for managing and developing applications
US20050228630A1 (en) * 1998-08-31 2005-10-13 Tseng Ping-Sheng VCD-on-demand system and method
US20030061541A1 (en) * 1999-06-03 2003-03-27 Kaler Christopher G. Method and apparatus for analyzing performance of data processing system
US6795963B1 (en) * 1999-11-12 2004-09-21 International Business Machines Corporation Method and system for optimizing systems with enhanced debugging information
US20110016358A1 (en) * 2007-09-14 2011-01-20 Airbus Operations (Societe Par Actions Simplifiee) Method for debugging operational software of a system onboard an aircraft and device for implementing the same
US8255875B2 (en) * 2008-09-30 2012-08-28 Rockwell Automation Technologies, Inc. Application builder for industrial automation

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
MathWorks, Simulink User Guide, 1990, page 2-15 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10747921B2 (en) 2016-01-05 2020-08-18 Cyient, Inc. Software tool for simulating operation of hardware and software systems
CN111060325A (en) * 2019-12-13 2020-04-24 斑马网络技术有限公司 Test scene construction method and device, electronic equipment and storage medium
CN111459369A (en) * 2020-04-13 2020-07-28 深圳康佳电子科技有限公司 Interface element screening method, intelligent terminal and storage medium

Also Published As

Publication number Publication date
US20120191443A1 (en) 2012-07-26
US20120192013A1 (en) 2012-07-26
US9020796B2 (en) 2015-04-28

Similar Documents

Publication Publication Date Title
US20120192158A1 (en) Model Based Verification Using Forward and Reverse Traversal of Variable Time Line
US6868508B2 (en) System and method enabling hierarchical execution of a test executive subsequence
US10360310B2 (en) Self-testing graphical component algorithm specification
US8429627B2 (en) Asynchronous preemptive edit time semantic analysis of a graphical program
US20050028107A1 (en) Editable data tooltips
US7076692B2 (en) System and method enabling execution stop and restart of a test executive sequence(s)
US7480826B2 (en) Test executive with external process isolation for user code modules
EP0869433A2 (en) A test development system and method for software with a graphical user interface
US8291390B2 (en) Testing a graphical program intended for a programmable hardware element
GB2272314A (en) Control sequencer in an Iconic Programming System
US20090012757A1 (en) Tools for system-level design environments
US11144434B2 (en) Refining coverage analyses using context information
WO2008021777A2 (en) Formal verification of graphical programs
US9495265B2 (en) Test executive system with processing of results data in chunks
US20030145252A1 (en) Test executive system having XML object representation capabilities
US20150339127A1 (en) Configuration Change Tracking for Measurement Devices
Campos et al. Supporting the analysis of safety critical user interfaces: an exploration of three formal tools
RU2678717C1 (en) Method for building a software system for automating and visualizing testing of embedded software for electronic devices
US20160357890A1 (en) Verification Log Analysis
US20030145280A1 (en) Test executive system having XML reporting capabilities
US7451358B2 (en) Test executive system with automatic expression logging and parameter logging
US20050049814A1 (en) Binding a GUI element to a control in a test executive application
US20040113947A1 (en) Operator interface controls for creating a run-time operator interface application for a test executive sequence
Biewald et al. EPOS-A specification and design technique for computer controlled real-time automation systems
US10235274B1 (en) Performing an action during program execution based on a dynamic condition

Legal Events

Date Code Title Description
AS Assignment

Owner name: CERTON SOFTWARE INC., FLORIDA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:STOCKTON, TIMOTHY;REEL/FRAME:028074/0800

Effective date: 20120410

AS Assignment

Owner name: CERTON SOFTWARE INC., FLORIDA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:AMALFITANO, CARLO;STOCKTON, TIMOTHY;MAROT, CHRISTOPHER;SIGNING DATES FROM 20150302 TO 20150306;REEL/FRAME:035123/0571

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION