CN104318105B - Effective sortie assessment method for aircraft flight trial - Google Patents

Effective sortie assessment method for aircraft flight trial Download PDF

Info

Publication number
CN104318105B
CN104318105B CN201410577603.8A CN201410577603A CN104318105B CN 104318105 B CN104318105 B CN 104318105B CN 201410577603 A CN201410577603 A CN 201410577603A CN 104318105 B CN104318105 B CN 104318105B
Authority
CN
China
Prior art keywords
flight test
sortie
flight
test subject
pilot fight
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.)
Expired - Fee Related
Application number
CN201410577603.8A
Other languages
Chinese (zh)
Other versions
CN104318105A (en
Inventor
李朝晖
李刚
蒋祖国
霍培锋
李昭广
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.)
Chinese Flight Test Establishment
Original Assignee
Chinese Flight Test Establishment
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 Chinese Flight Test Establishment filed Critical Chinese Flight Test Establishment
Priority to CN201410577603.8A priority Critical patent/CN104318105B/en
Publication of CN104318105A publication Critical patent/CN104318105A/en
Application granted granted Critical
Publication of CN104318105B publication Critical patent/CN104318105B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention provides an effective sortie assessment method for aircraft flight trial. The method includes: respectively adopting two calculation methods according to the fact whether the aircraft a trial flight belongs to a comprehensive test subject or a single test subject to acquire success rate of a flight trial sortie; judging whether the trial flight is the effective sortie or not according to the threshold of the success rate. In the method, interference of artificial subjective factors and more external environment factors can be eliminated as much as possible, and effectiveness of the aircraft flight trial sortie is assessed scientifically, quantitatively and objectively; a flight trial list is standardized, trial flight contents are scientifically and reasonably demanded and arranged, driving techniques of the trial flight are accurately mastered, the test methods and instruments are used correctly, reliability in maintenance and field work guarantee is improved, collaboration of flight trial engineers and trial pilots is enhanced, and test efficiency and effectiveness of the aircraft flight trial are improved.

Description

Aircraft flight test effective sortie assessment method
Technical field
The invention belongs to aircraft experimental technique field, specially a kind of aircraft flight test effective sortie evaluation side Method, is scientifically judged for the effectiveness of flight test sortie in airborne vehicle airflight test.
Background technology
Flight test is the scientific experimentss activity carried out under Live Flying environmental condition.Flight test is once to test What flight was counted as elementary cell, the flight of flight test is commonly referred to a flight test sortie, abbreviation one Take a flight test sortie.For the validity check process of flight test parameter raw data, a sortie of taking a flight test actually is evaluated Effectiveness, that is, the evaluation of effective sortie of taking a flight test.Effective sortie of taking a flight test is evaluated, effective sortie of taking a flight test accordingly must be just formulated The method of evaluation.
Effective sortie of taking a flight test evaluation is a requisite important step, its purpose in any flight test problem activity Be to ensure that sortie quality of taking a flight test, be test mission complete take a firm foundation, the quality assurance tool to the problem that completes to take a flight test It is significant.
At present, it is still no in air weapon flight test procedure link at home to comment with regard to flight test effective sortie Fixed theory, method and assessment criteria.Do not embody in the national military standard promulgated yet and commented with regard to flight test effective sortie Fixed relatedness standard or clause.
The content of the invention
It is an object of the invention to provide the method for complete set is used to evaluate the effective sortie of flight test, the method wants energy Enough interference for excluding artificial subjective factor and more outside environmental elements as much as possible, science, it is quantitative, objectively evaluate airborne vehicle The effectiveness of flight test sortie.So as to specification test mission single pair of take a flight test content require with arrange scientific rationality, to examination The accurate assurance of winged driving technology, to the proper use of of method of testing and instrument, and improve the reliability that engineering and floor manager ensure Property, reinforcement is taken a flight test the cooperateing with of engineer and test pilot, raising aircraft test efficiency and benefit.
The technical scheme is that:
A kind of aircraft flight test effective sortie assessment method, it is characterised in that:Comprise the following steps:
Step 1:Collection pilot fight parameter of taking a flight test, and judge this pilot fight be single flight test subject or Combined flight test subject, if combined flight test subject, into step 2, if single flight test subject, into step 3;
Step 2:This pilot fight be combined flight test subject, this pilot fight take a flight test sortie success rate FTVA according to Below equation is calculated:
Wherein FTVAKiFor the success rate of i-th flight test subject, m is the flight test subject quantity that this pilot fight is included, Qi Weighted value corresponding to i-th flight test subject, and Q1+Q2+…Qi+…+Qm=1;
Success rate FTVAK of flight test subject is calculated according to below equation:
Wherein pkFor the qualification rate of k-th action of the flight test subject, pk∈ [0,1], n are the action that the flight test subject is included Number, qkFor the weighted value of k-th action of the flight test subject, and q1+q2+…qk+…+qn=1;
Step 3:This pilot fight be single flight test subject, this pilot fight take a flight test sortie success rate FTVA according to Below equation is calculated:
Wherein pAiFor the qualification rate of i-th action element of the pilot fight, pAi∈ [0,1], u are included for the pilot fight Action element number, qAiFor the weighted value of i-th action element of the pilot fight, and qA1+qA2+…qAi+…+qAu=1;
Step 4:For the purpose pilot fight of combined flight test section, if sortie success rate FTVA of taking a flight test of this pilot fight >= 0.6, then this pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, and have at least Success rate FTVAK >=0.6 of one of flight test subject, then this pilot fight is part effective sortie;If this test flies The capable sortie success rate FTVA < 0.6 that takes a flight test, and the success rate FTVAK < 0.6 of each flight test subject, then this pilot fight be Noneffective sortie;For the pilot fight of single flight test subject, if sortie success rate FTVA >=0.6 of taking a flight test of this pilot fight, Then this pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, this test flies Behavior noneffective sortie.
For the single flight test subject pilot fight of step 3, the examination of this pilot fight can also be calculated using below equation Arch high over time success rate FTVA:
Wherein pBiFor the qualification rate of i-th flight parameter of the pilot fight, pBi∈ [0,1], v are to need in the pilot fight The flight parameter number to be passed judgment on, qBiFor the weighted value of i-th flight parameter, and qB1+qB2+…qBi+…+qBv=1.
Further preferred version, a kind of aircraft flight test effective sortie assessment method, it is characterised in that:Flight The qualification rate of action and/or flight parameter is divided into Three Estate according to the evaluation criterion of national military standard, and wherein good degree correspondence is closed Lattice rate value is [0.9,1], and qualified grade corresponds to qualification rate value for [0.6,0.9), unqualified grade corresponds to qualification rate value For [0,0.6).
Further preferred version, a kind of aircraft flight test effective sortie assessment method, it is characterised in that:Flight The qualification rate of action and/or flight parameter is divided into Three Estate according to the evaluation criterion of national military standard, and wherein good degree correspondence is closed Lattice rate value is 1, and qualified grade correspondence qualification rate value is 0.6, and unqualified grade correspondence qualification rate value is 0.
Further preferred version, a kind of aircraft flight test effective sortie assessment method, it is characterised in that:According to The flight parameter for needing to pass judgment on is divided into key parameter, important parameter and general parameterss by the importance in pilot fight, The weighted value of key parameter is more than the weighted value of important parameter, and the weighted value of important parameter is more than the weighted value of general parameterss, winged The weighted value of line parameter is maximum to be not more than 0.5, and minimum is not less than 0.05.
Further preferred version, a kind of aircraft flight test effective sortie assessment method, it is characterised in that:It is crucial The weighted value of parameter and for 0.5, the weighted value of important parameter and for 0.3, the weighted value of general parameterss and for 0.2.
Beneficial effect
The invention has the beneficial effects as follows:Domestic flight test field is filled up and has lacked quantitative assessment always and taken a flight test effective sortie The blank of method, has by having filled up in the present invention at home air weapon flight test procedure link with regard to flight test Theory, method and assessment criteria that effect sortie is evaluated.Sortie quantization assessment method of taking a flight test determined by the present disclosure, for raising Take a flight test efficiency, reduction take a flight test cost, the process of taking a flight test of refining, shortening take a flight test the cycle, solve in the past artificial subjective evaluation and take a flight test sortie Validity problem is respectively provided with Practical Project value.
Description of the drawings
Fig. 1:Flight test effective sortie evaluates operational flowchart.
Specific embodiment
With reference to the specific embodiment description present invention:
In flight test, flight test effective sortie refers to test pilot, take a flight test engineer and support personnel's foundation of taking a flight test The test mission list of approval, by flight test subject requirement the flight of scientific research or training test mission is completed.In the present invention, in order to To taking a flight test, effective sortie carries out Quantitative evaluation, employs the effectiveness that sortie success rate of taking a flight test represents sortie of taking a flight test.Take a flight test sortie Success rate refers to some numerical value between 0 and 1, and when success rate standard of the numerical value more than or equal to setting, then this is taken a flight test Sortie is effectively, otherwise invalid.If success rate thresholding is represented with [W], sortie success rate of taking a flight test is represented by W ∈ [0,1].
1st, take a flight test effective sortie Universal Criterion and rating
It is determined that effective sortie Universal Criterion of taking a flight test it is as follows:
FTVA >=[W] is effectively
FTVA < [W] invalid (1)
In formula:FTVA refers to sortie effectiveness evaluation score value (or success rate) of taking a flight test, and [W] refers to sortie success rate thresholding of taking a flight test Value, generally takes [W]=0.6.
The rating of flight test effective sortie divides as follows:
Effective sortie is divided into:It is outstanding:FTVA >=90%;It is qualified:60%≤FTVA < 90%;Part effective sortie[note]:Extremely FTVAK >=60% of few one of flight test subject;Noneffective sortie:The FTVAK < 60% of each flight test subject;In formula:FTVAK Refer to flight test subject success rate.
[note]:It is only applicable to " combined flight test sortie ".
The evaluation of flight test effective sortie is completed by evaluating flight test subject, the evaluation of flight test subject effectiveness Take a flight test action to complete by evaluation, and one is taken a flight test what action typically took a flight test parameter to characterize by one group.Therefore, it is Evaluation flight test subject, it is necessary to which the relevant parameter for choosing the action of taking a flight test in correspondence flight test subject is most basic as object is passed judgment on Element, should be chosen for completing the parameter of taking a flight test that certain sortie flight test subject plays a major role in principle.The flight test of one sortie Can be single section's purpose take a flight test, or multiple subjects composition combined flight test.
2nd, flight test subject success rate computing formula is as follows
In formula
The action number that n-flight test subject is included
pkThe qualification rate of-k-th action, k=1 ..., n
qkThe weighted value of-k-th action, and
q1+q2+…qk+…+qn=1 (3)
The weighted value of action of taking a flight test refers to that the examination of the action of taking a flight test, to completing the significance level of flight flight test subject, needs It is previously set.When being difficult to determine the degree of action performance assessment criteria importance of respectively taking a flight test, can adopt etc. power process method.
The evaluation of driver behavior qualification rate can refer to national military standard GJB 624A-2010《Military aircraft scientific research is taken a flight test training requirement》 In " evaluation criterion ".For the flight test subject for having clear and definite index request in test mission list, test mission list should be preferentially selected Specified in index.
Reach for same flight test subject requires repeatedly to take a flight test in test mission list and once requirement of taking a flight test Action, its effectiveness score of the examination is once defined by best.
3rd, sortie success rate computing formula of taking a flight test is as follows
In formula
FTVAKiThe success rate of-i-th flight test subject, i=1,2 ..., m
QiWeighted value corresponding to-i-th flight test subject, and
Q1+Q2+…Qi+…+Qm=1 (5)
The flight test subject quantity that m-sortie of taking a flight test includes
The weighted value of each flight test subject depends on the importance and crucial journey of each flight test subject for decomposing in formula (5) Degree, needs to be previously set.Success rate FTVAK of each flight test subject is calculated by formula (2).
4th, sortie success rate of taking a flight test is calculated according to flare maneuver qualification rate as follows
This flight has n main flare maneuver element, and the qualification rate of each action element is pAi, shared by each action Weigh as qAi, then success rate FTVA of this flightAIt is represented by
In formula
qA1+qA2+…+qAi+…+qAn=1 (8)
Power q of each action in formula (6)AiIt is to be previously set according to the criticality of action, pAiIt is to each action Acceptable level by being given after above-mentioned national military standard prejudgementing criteria analysis, if the action is excellent, pAi=1, the action is qualified, then pAi =0.6, the action is unqualified, then pAi=0.
Excellent P in formula (7)Ai=1 is the upper limit for having taken good degree (0.9~1), qualified to take pAi=0.6 is to have taken conjunction The lower limit of lattice grade (0.6~0.9), unqualified pAi=0, take the lower limit of unqualified grade (0~0.6).So both it is easy to take Value, has certain reasonability again.
This flight success rate FTVA can be calculated by formula (6)A, and substitute into take a flight test in effective sortie Universal Criterion formula (1), with Success rate standard [W] is compared, you can judge whether the sortie of taking a flight test is effective.
5th, sortie success rate of taking a flight test is calculated according to flight parameter qualification rate as follows
When flight is made up of a flight test subject, can be passed judgment on using flight parameter.Flight parameter pass judgment on form with Flare maneuver passes judgment on similar, only flare maneuver need to be transformed into into main flight parameter, uses FTVABRepresent that flight parameter is passed judgment on Flight success rate, then
In formula
pBi--- i-th flight parameter qualification rate
I --- flight parameter number, i=1,2 ..., n
qBi--- the power shared by i-th flight parameter
qB1+qB2+……+qBi+……+qBn=1 (11)
6th, type choosing method is passed judgment on
Judge type is chosen according to object is passed judgment on.Passing judgment on object has two layers of meaning:One refers to that this flight is single examination Winged subject or combined flight test subject, two refer to flare maneuver still with flight parameter as main judge object.
If single flight test subject, then choose flare maneuver and pass judgment on class pattern (6) or flight parameter judge class pattern (9) To calculate success rate FTVA, if combined flight test subject, then choose combined flight test subject and pass judgment on class pattern (4) to calculate successfully Rate FTVA;If using flare maneuver as main judge object, choosing formula (6), if using flight parameter as main judge object, Then choose formula (9).
Either choose flare maneuver and pass judgment on formula (6) or flight parameter judge formula (9), final judge object elements are all It is flight parameter, only formula (6) is that, using flare maneuver as main judge object, and formula (9) is commented as master using flight parameter Sentence object, in whole flight, flight parameter number is substantially constant after selecting, only in difference Flare maneuver in flight parameter emphasis it is different, play a crucial role to the action success or failure several are only selected in a certain action It is individual until one or two parameter, and mainly Quantitative evaluation.
Letting us choose up to see flare maneuver judge class pattern (6) still selects flight parameter to pass judgment on class pattern (9), and this wants concrete condition Concrete analysis.If taking based on aerial main actions segment data to pass judgment on sortie effectiveness of taking a flight test, it is proposed that select formula (6);If Take one completely to rise and fall data to pass judgment on sortie effectiveness of taking a flight test, it is proposed that select formula (9).
7th, the determination method of element weighted value
Select and pass judgment on it is necessary to determine element number, elementary composition and element the weight ratio of passing judgment on object after type, this One process of sample is referred to as element power and determines.It is assumed that choosing flight parameter passes judgment on formula (9), then element weighting is determined as follows Value:
1) element number is chosen
It is flight parameter that flight parameter passes judgment on the judge object elements of formula (9), should be found out to complete the flight test subject task Those flight parameters for playing a major role.For each intensity flight test subject, these flight parameters are included but is not limited to: Flight speed (V), flying height (h), three-dimensional overload (nz、nx、ny), the angle of attack (α), yaw angle (β), three-dimensional manipulate displacement (de、 da、dr), three angle of rudder reflection (δe、δa、δr).The main flight parameter of the flight test subject should be found out from these flight parameters, typically For, preferably not more than 8.
2) determine elementary composition
Have chosen it is elementary composition it is necessary to determine after the param elements number of this flight, typically by key element, important unit Element and general element composition.Key element refers to the element played a crucial role to this flight success or failure, and key element number is few, but rises Pivotal role, important element is less, plays an important role, and general element is more, plays a secondary role.For example it is assumed that have selected 8 flying Line parameter then may be selected 1~2 key element as the element of this flight, 2~3 important elements, and remaining is general unit Element.
3) determine that element weights compare qi
Determine it is elementary composition after weight ratio q of each element is determined by three ingredients of elementi, determine qiShould abide by Follow following principle:
(1) determine that element is weighed by the significance level of element, than bigger, vice versa for more crucial element weights.
(2) power of most critical element is not more than 0.5, and the least power of important element is not less than 0.05.
(3) all elements power sum is equal to 1.
8th, element qualification rate obtaining value method
Every kind of element qualification rate piCan be with one of following methods come value:
1) extreme value is taken
According to national military standard, element qualification rate is divided into excellent, qualified and unqualified Three Estate, the value model of each grade Enclose and be shown below
It is so-called take extreme value and just refer to maximum (upper limit) or minimum (lower limit) are according to circumstances taken in each rate range, Excellent level takes its maximum p1=1, regular grade and unqualified level difference minimalization (lower limit), i.e., regular grade takes p2=0.6, no Regular grade takes p3=0, such benefit one is convenient, and two is that each grade differential is obvious, there is certain reasonability.
2) treating excess syndrome border estimated value
So-called treating excess syndrome border estimated value, refers to by the practical situation in three qualification rate rate ranges choose estimated value, example Such as, certain element belongs to qualified grade according to the Changing Pattern and size of the parameter, occupies upper middle again in the rate range, i.e., Can use qualification rate p of the parameter2For certain value between 0.8~0.9, p is such as taken2=0.88;If occupying lower middle can use p2 For certain value between 0.6~0.7, p is such as taken2=0.62.Although this obtaining value method comparison is rationally, cumbersome.
Analyze according to more than, and with reference to the accompanying drawings 1, obtain concretely comprising the following steps for the present embodiment:
Step 1:Collection pilot fight parameter of taking a flight test, and judge this pilot fight be single flight test subject or Combined flight test subject, if combined flight test subject, into step 2, if single flight test subject, into step 3.
Step 2:This pilot fight be combined flight test subject, this pilot fight take a flight test sortie success rate FTVA according to Below equation is calculated:
Wherein FTVAKiFor the success rate of i-th flight test subject, m is the flight test subject quantity that this pilot fight is included, Qi Weighted value corresponding to i-th flight test subject, and Q1+Q2+…Qi+…+Qm=1;
Success rate FTVAK of flight test subject is calculated according to below equation:
Wherein pkFor the qualification rate of k-th action of the flight test subject, pk∈ [0,1], n are the action that the flight test subject is included Number, qkFor the weighted value of k-th action of the flight test subject, and q1+q2+…qk+…+qn=1;
Step 3:This pilot fight be single flight test subject, this pilot fight take a flight test sortie success rate FTVA according to Below equation is calculated:
Wherein pAiFor the qualification rate of i-th action element of the pilot fight, pAi∈ [0,1], u are included for the pilot fight Action element number, qAiFor the weighted value of i-th action element of the pilot fight, and qA1+qA2+…qAi+…+qAu=1;
For example certain maneuvering flight sortie is made up of 5 major motor actions, action serial number k, each action and each The qualification rate of time period parameter testing corresponding to action is pAk, weighted value q shared by itAk, as shown in table 1.
The action qualification rate and action weighted value of table 1 certain maneuvering flight sortie
Action sequence number k 1 2 3 4 5
Action qualification rate pAk 1 1 1 0.6 0.0
Action weighted value qAk 0.4 0.3 0.1 0.1 0.1
The effectiveness for calculating the maneuvering flight sortie is as follows:
FTVA=1 × 0.4+1 × 0.3+1 × 0.1+0.6 × 0.1+0.0 × 0.1
=0.4+0.3+0.1+0.06+0
=86% (regular grade, effective sortie)
Divided according to above-mentioned flight test effective sortie rating and understood, the motor-driven flight test subject of the sortie belongs to regular grade Effectively take a flight test sortie.
For single flight test subject, sortie success rate FTVA of taking a flight test of pilot fight is calculated always according to below equation:
Wherein pBiFor the qualification rate of i-th flight parameter of the pilot fight, pBi∈ [0,1], v are to need in the pilot fight The flight parameter number to be passed judgment on, qBiFor the weighted value of i-th flight parameter, and qB1+qB2+…qBi+…+qBv=1.
Here, for the qualification rate and the qualification rate of flight parameter of action, according to the evaluation criterion of national military standard three are divided into Individual grade, wherein good degree correspondence qualification rate value is [0.9,1], qualified grade correspondence qualification rate value for [0.6,0.9), Unqualified grade correspondence qualification rate value is for [0,0.6).According to above-mentioned analysis, the present embodiment is using bounding method is taken, i.e., excellent Grade correspondence qualification rate value is 1, and qualified grade correspondence qualification rate value is 0.6, and unqualified grade correspondence qualification rate value is 0。
And for using need pass judgment on flight parameter calculate pilot fight take a flight test sortie success rate when, according to test The flight parameter for needing to pass judgment on is divided into key parameter, important parameter and general parameterss, key ginseng by aloft importance Several weighted values is more than the weighted value of important parameter, and the weighted value of important parameter is more than the weighted value of general parameterss, flight parameter Weighted value it is maximum be not more than 0.5, minimum is not less than 0.05.Further, the weighted value of key parameter and for 0.5, important ginseng Several weighted value and for 0.3, the weighted value of general parameterss and for 0.2.
Such as strength of aircraft pilot fight, can from flight speed (V), flying height (h), three-dimensional overload (nz, nx, Ny), the angle of attack (α), yaw angle (β), three-dimensional are manipulated in the performance parameters such as displacement (de, da, dr), three angle of rudder reflection (δ e, δ a, δ r) Choose the flight parameter for needing to pass judgment on.8 are not typically exceeded.It is assumed that have selected 8 flight parameters as this pilot fight Need the flight parameter passed judgment on, then according to the importance in pilot fight, select 1~2 key element, 2~3 important units Element, remaining is general element, such as table 2.
Table 2 determines weighter factor example
Step 4:Based on above-mentioned calculating, for the purpose pilot fight of combined flight test section, if the frame of taking a flight test of this pilot fight Secondary success rate FTVA >=0.6, then this pilot fight is effective sortie;If sortie success rate FTVA of taking a flight test of this pilot fight < 0.6, and have success rate FTVAK >=0.6 of at least one of which flight test subject, then this pilot fight is part effectively frame It is secondary;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, and the success rate FTVAK < 0.6 of each flight test subject, Then this pilot fight is noneffective sortie;For the pilot fight of single flight test subject, if the sortie of taking a flight test of this pilot fight Success rate FTVA >=0.6, then this pilot fight is effective sortie;If the sortie success rate FTVA < that takes a flight test of this pilot fight 0.6, then this pilot fight is noneffective sortie.

Claims (6)

1. a kind of aircraft flight test effective sortie assessment method, it is characterised in that:Comprise the following steps:
Step 1:The parameter of taking a flight test of pilot fight of collection, and judge that this pilot fight is single flight test subject or synthesis Flight test subject, if combined flight test subject, into step 2, if single flight test subject, into step 3;
Step 2:This pilot fight is combined flight test subject, and sortie success rate FTVA of taking a flight test of this pilot fight is according to following Formula is calculated:
F T V A = Σ i = 1 m FTVAK i Q i
Wherein FTVAKiFor the success rate of i-th flight test subject, m is the flight test subject quantity that this pilot fight is included, QiFor Weighted value corresponding to i flight test subject, and Q1+Q2+…Qi+…+Qm=1;
Success rate FTVAK of flight test subject is calculated according to below equation:
F T V A K = Σ k = 1 n p k q k
Wherein pkFor the qualification rate of k-th flare maneuver of the flight test subject, pk∈ [0,1], n are the flight that the flight test subject is included Action number, qkFor the weighted value of k-th flare maneuver of the flight test subject, and q1+q2+…qk+…+qn=1;
Step 3:This pilot fight is single flight test subject, and sortie success rate FTVA of taking a flight test of this pilot fight is according to following Formula is calculated:
F T V A = p A 1 q A 1 + p A 2 q A 2 + ... p A i q A i + ... + p A u q A u = Σ i = 1 u p A i q A i
Wherein pAiFor the qualification rate of i-th flare maneuver element of the pilot fight, pAi∈ [0,1], u are that the pilot fight is included Flare maneuver element number, qAiFor the weighted value of i-th flare maneuver element of the pilot fight, and qA1+qA2+…qAi+…+qAu =1;
Step 4:For the purpose pilot fight of combined flight test section, if sortie success rate FTVA >=0.6 of taking a flight test of this pilot fight, Then this pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, and have at least within Success rate FTVAK >=0.6 of one flight test subject, then this pilot fight is part effective sortie;If this pilot fight Sortie success rate FTVA of taking a flight test < 0.6, and the success rate FTVAK < 0.6 of each flight test subject, then this pilot fight is invalid Sortie;For the pilot fight of single flight test subject, if sortie success rate FTVA >=0.6 of taking a flight test of this pilot fight, should Secondary pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, this pilot fight is Noneffective sortie.
2. a kind of aircraft flight test effective sortie assessment method, it is characterised in that:Comprise the following steps:
Step 1:The parameter of taking a flight test of pilot fight of collection, and judge that this pilot fight is single flight test subject or synthesis Flight test subject, if combined flight test subject, into step 2, if single flight test subject, into step 3;
Step 2:This pilot fight is combined flight test subject, and sortie success rate FTVA of taking a flight test of this pilot fight is according to following Formula is calculated:
F T V A = Σ i = 1 m FTVAK i Q i
Wherein FTVAKiFor the success rate of i-th flight test subject, m is the flight test subject quantity that this pilot fight is included, QiFor Weighted value corresponding to i flight test subject, and Q1+Q2+…Qi+…+Qm=1;
Success rate FTVAK of flight test subject is calculated according to below equation:
F T V A K = Σ k = 1 n p k q k
Wherein pkFor the qualification rate of k-th flare maneuver of the flight test subject, pk∈ [0,1], n are the flight that the flight test subject is included Action number, qkFor the weighted value of k-th flare maneuver of the flight test subject, and q1+q2+…qk+…+qn=1;
Step 3:This pilot fight is single flight test subject, and sortie success rate FTVA of taking a flight test of this pilot fight is according to following Formula is calculated:
F T V A = Σ i = 1 v p B i q B i
Wherein pBiFor the qualification rate of i-th flight parameter of the pilot fight, pBi∈ [0,1], v are to need to comment in the pilot fight The flight parameter number sentenced, qBiFor the weighted value of i-th flight parameter, and qB1+qB2+…qBi+…+qBv=1;
Step 4:For the purpose pilot fight of combined flight test section, if sortie success rate FTVA >=0.6 of taking a flight test of this pilot fight, Then this pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, and have at least within Success rate FTVAK >=0.6 of one flight test subject, then this pilot fight is part effective sortie;If this pilot fight Sortie success rate FTVA of taking a flight test < 0.6, and the success rate FTVAK < 0.6 of each flight test subject, then this pilot fight is invalid Sortie;For the pilot fight of single flight test subject, if sortie success rate FTVA >=0.6 of taking a flight test of this pilot fight, should Secondary pilot fight is effective sortie;If the sortie success rate FTVA < 0.6 that takes a flight test of this pilot fight, this pilot fight is Noneffective sortie.
3. a kind of aircraft flight test effective sortie assessment method according to claim 1 or claim 2, it is characterised in that:Flight is dynamic Make and/or the qualification rate of flight parameter is divided into Three Estate according to the evaluation criterion of national military standard, wherein good degree correspondence is qualified Rate value is [0.9,1], and qualified grade correspondence qualification rate value is for [0.6,0.9), unqualified grade correspondence qualification rate value is [0,0.6)。
4. a kind of aircraft flight test effective sortie assessment method according to claim 3, it is characterised in that:Flare maneuver And/or the qualification rate of flight parameter is divided into Three Estate, wherein good degree correspondence qualification rate according to the evaluation criterion of national military standard Value is 1, and qualified grade correspondence qualification rate value is 0.6, and unqualified grade correspondence qualification rate value is 0.
5. a kind of aircraft flight test effective sortie assessment method according to claim 2, it is characterised in that:According in test The flight parameter for needing to pass judgment on is divided into key parameter, important parameter and general parameterss, key ginseng by aloft importance Several weighted values is more than the weighted value of important parameter, and the weighted value of important parameter is more than the weighted value of general parameterss, flight parameter Weighted value it is maximum be not more than 0.5, minimum is not less than 0.05.
6. a kind of aircraft flight test effective sortie assessment method according to claim 5, it is characterised in that:Key parameter Weighted value and for 0.5, the weighted value of important parameter and for 0.3, the weighted value of general parameterss and for 0.2.
CN201410577603.8A 2014-10-24 2014-10-24 Effective sortie assessment method for aircraft flight trial Expired - Fee Related CN104318105B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410577603.8A CN104318105B (en) 2014-10-24 2014-10-24 Effective sortie assessment method for aircraft flight trial

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410577603.8A CN104318105B (en) 2014-10-24 2014-10-24 Effective sortie assessment method for aircraft flight trial

Publications (2)

Publication Number Publication Date
CN104318105A CN104318105A (en) 2015-01-28
CN104318105B true CN104318105B (en) 2017-04-19

Family

ID=52373336

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410577603.8A Expired - Fee Related CN104318105B (en) 2014-10-24 2014-10-24 Effective sortie assessment method for aircraft flight trial

Country Status (1)

Country Link
CN (1) CN104318105B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2795529C1 (en) * 2022-12-30 2023-05-04 Акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Flying laboratory with a reconfigurable test-pilot workplace for advanced flight studies of the “crew-automatic” and “crew-uav” interaction

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104680325A (en) * 2015-03-09 2015-06-03 中国航空工业集团公司沈阳飞机设计研究所 Automatic UAV (unmanned aerial vehicle) flight test task list planning method on basis of Oracle database
CN110505294B (en) * 2019-08-20 2021-09-14 上海航空工业(集团)有限公司 Method for automatically distributing test flight data files
CN112101647B (en) * 2020-09-04 2023-06-23 西北工业大学 Multi-objective optimization method for civil transportation airplane flight test efficiency
CN112686523A (en) * 2020-12-25 2021-04-20 中国航空工业集团公司沈阳飞机设计研究所 Flight quality assessment method and system for airplane to execute closed-loop maneuvering task
CN116383975B (en) * 2023-06-06 2023-08-15 西北工业大学 Landing gear load prediction method based on test flight data

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102363448A (en) * 2011-08-25 2012-02-29 中国商用飞机有限责任公司 Experiment method of flight simulator
US8204637B1 (en) * 2007-12-20 2012-06-19 The United States Of America As Represented By The Secretary Of The Navy Aircraft approach to landing analysis method
CN102938020A (en) * 2012-10-26 2013-02-20 哈尔滨工程大学 Aircraft landing efficiency estimating method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8204637B1 (en) * 2007-12-20 2012-06-19 The United States Of America As Represented By The Secretary Of The Navy Aircraft approach to landing analysis method
CN102363448A (en) * 2011-08-25 2012-02-29 中国商用飞机有限责任公司 Experiment method of flight simulator
CN102938020A (en) * 2012-10-26 2013-02-20 哈尔滨工程大学 Aircraft landing efficiency estimating method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
基于扩展的FMC实物试验用于飞行仿真和飞行试验;李朝晖等;《中国民航大学学报》;20081031;第26卷(第5期);第60-65页 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2795529C1 (en) * 2022-12-30 2023-05-04 Акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Flying laboratory with a reconfigurable test-pilot workplace for advanced flight studies of the “crew-automatic” and “crew-uav” interaction

Also Published As

Publication number Publication date
CN104318105A (en) 2015-01-28

Similar Documents

Publication Publication Date Title
CN104318105B (en) Effective sortie assessment method for aircraft flight trial
Loeb et al. Accountability and local control: Response to incentives with and without authority over resource generation and allocation
CN104537211A (en) Enterprise safety risk early warning method based on analytic hierarchy process and grey theory
CN110160789A (en) A kind of Wind turbines Method for Bearing Fault Diagnosis based on GA-ENN
CN107766668A (en) A kind of complex simulation model verification method based on neutral net
CN105931153A (en) Indirect questionnaire assessment method based on neural network prediction analysis model
CN102568267A (en) Computer online examination method
CN104318110A (en) Method for improving risk design and maintenance efficiency of large complex system on basis of importance and sensibility complex sequence
CN106056274A (en) Power construction main body benefit analysis method based on PCA-DEA two-dimensional comprehensive evaluation model
CN106530843A (en) Student experiment comprehensive evaluation method based on online laboratory
Akin Arikan A Comparison of Kernel Equating Methods Based on Neat Design.
CN107300907A (en) With reference to the flight control system Reliable Evaluating Methods of Their Performance of comprehensive assessment and hypothesis testing
CN111369140B (en) Teaching evaluation system and method
CN105740237A (en) Lexical semantic similarity based student ability achievement degree evaluation measurement method
Acar Measurement of Attitudes Regarding Foreign Language Skills and Its Relation with Success.
Hamada et al. Bayesian binomial assurance tests for system reliability using component data
You et al. Prospective elementary and middle school teachers’ knowledge of linear functions: A quantitative approach
CN106709642A (en) Air traffic control simulation training evaluation method
Rohim et al. Analysis of the effect of occupational safety and health (K3) on employee performance in distribution center area logistics division
Dozortsev et al. Evaluation of the Process Operator Knowledge Formation Resulting from Computer-Based Training
CN112150886A (en) Method for evaluating validity of data package test flight data of flight simulator
Huang et al. RESEARCH ON INDEPENDENT COLLEGE TEACHERS’TEACHING ABILITY BASED ON FACTOR ANALYSIS IN SPSS
CN108764687A (en) A kind of method and its system of assessment construction safety management performance
Li et al. The evaluation model of psychological quality for civil aviation student pilot based on fuzzy comprehensive evaluation
Yin et al. Study on Virtual Maintenance Training Effect Evaluation Based on Cognitive

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170419

Termination date: 20171024