DE69602798T2 - Satelliten Drallstabilisationsverfahren, in dem ein transversales Trägheitsmoment mit einem einzigen Freiheitsgrad gespeichert wird, und System dazu - Google Patents

Satelliten Drallstabilisationsverfahren, in dem ein transversales Trägheitsmoment mit einem einzigen Freiheitsgrad gespeichert wird, und System dazu

Info

Publication number
DE69602798T2
DE69602798T2 DE69602798T DE69602798T DE69602798T2 DE 69602798 T2 DE69602798 T2 DE 69602798T2 DE 69602798 T DE69602798 T DE 69602798T DE 69602798 T DE69602798 T DE 69602798T DE 69602798 T2 DE69602798 T2 DE 69602798T2
Authority
DE
Germany
Prior art keywords
inertia
satellite
freedom
stored
stabilization method
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 - Lifetime
Application number
DE69602798T
Other languages
English (en)
Other versions
DE69602798D1 (de
Inventor
Richard A Fowell
John F Yocum
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69602798D1 publication Critical patent/DE69602798D1/de
Publication of DE69602798T2 publication Critical patent/DE69602798T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
DE69602798T 1995-04-28 1996-04-18 Satelliten Drallstabilisationsverfahren, in dem ein transversales Trägheitsmoment mit einem einzigen Freiheitsgrad gespeichert wird, und System dazu Expired - Lifetime DE69602798T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/430,636 US5667171A (en) 1995-04-28 1995-04-28 Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device

Publications (2)

Publication Number Publication Date
DE69602798D1 DE69602798D1 (de) 1999-07-15
DE69602798T2 true DE69602798T2 (de) 2000-01-27

Family

ID=23708400

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69602798T Expired - Lifetime DE69602798T2 (de) 1995-04-28 1996-04-18 Satelliten Drallstabilisationsverfahren, in dem ein transversales Trägheitsmoment mit einem einzigen Freiheitsgrad gespeichert wird, und System dazu

Country Status (4)

Country Link
US (3) US5667171A (de)
EP (1) EP0739818B1 (de)
BR (1) BR9602020A (de)
DE (1) DE69602798T2 (de)

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US6062512A (en) * 1997-08-27 2000-05-16 Hughes Electronics Corporation Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices
US6162123A (en) 1997-11-25 2000-12-19 Woolston; Thomas G. Interactive electronic sword game
US6128556A (en) * 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
US6152403A (en) * 1998-11-11 2000-11-28 Hughes Electronics Corporation Gyroscopic calibration methods for spacecraft
US6202007B1 (en) * 1999-02-19 2001-03-13 John A. Spicer Exact stability integration in network designs
US6463365B1 (en) * 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft
US7074175B2 (en) 2001-07-25 2006-07-11 Erik Schroeder Handy Thermotherapy via targeted delivery of nanoscale magnetic particles
US6860451B1 (en) * 2003-11-21 2005-03-01 The Boeing Company Spacecraft spin axis reorientation method
US20050133670A1 (en) * 2003-12-03 2005-06-23 Wang H. G. Unified sensor-based attitude determination and control for spacecraft operations
US7665695B2 (en) * 2003-12-03 2010-02-23 The Boeing Company Unified attitude control for spacecraft transfer orbit operations
US7603424B2 (en) * 2005-11-03 2009-10-13 Research In Motion Limited Method and system for generating template replies to electronic mail messages
EP1951906B1 (de) * 2005-11-10 2010-12-22 Bristol-Myers Squibb Pharma Company Moesin, caveolin 1 und yes-assoziiertes protein 1 als prädiktive marker der reaktion auf dasatinib bei brustkrebs
JP5030811B2 (ja) * 2008-02-15 2012-09-19 三菱重工業株式会社 宇宙機システム
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
FR2937954B1 (fr) * 2008-10-31 2011-07-29 Thales Sa Procede et systeme de desaturation des roues d'inertie d'un engin spatial
US8014911B2 (en) * 2009-11-03 2011-09-06 Honeywell International Inc. Methods and systems for imposing a momentum boundary while reorienting an agile vehicle with control moment gyroscopes
RU2481250C1 (ru) * 2011-12-28 2013-05-10 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Система стабилизации углового движения космического аппарата
FR3013685B1 (fr) 2013-11-25 2017-05-19 Astrium Sas Procede et dispositif de commande d'une phase d'acquisition du soleil par un engin spatial
US10050491B2 (en) 2014-12-02 2018-08-14 Management Services Group, Inc. Devices and methods for increasing energy and/or power density in composite flywheel energy storage systems
US9573623B2 (en) * 2015-01-08 2017-02-21 GM Global Technology Operations LLC Collision avoidance control integrated with electric power steering controller and rear steer
EA028853B1 (ru) * 2015-07-07 2018-01-31 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ пространственной переориентации и изменения параметров углового движения космического аппарата
US10144531B2 (en) 2016-02-04 2018-12-04 The Boeing Company Reorientation of a spinning spacecraft using gimbaled electric thrusters
US9963248B2 (en) * 2016-02-04 2018-05-08 The Boeing Company Spin stabilization of a spacecraft for an orbit maneuver
US11279501B2 (en) * 2018-10-25 2022-03-22 General Atomics Satellite attitude control system using eigen vector, non-linear dynamic inversion, and feedforward control
CN116280275B (zh) * 2023-01-19 2024-03-19 中国科学院微小卫星创新研究院 一种角动量自守恒机构以及卫星

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US3591108A (en) * 1967-01-27 1971-07-06 Rca Corp Control system for spinning bodies
US3637170A (en) * 1969-12-31 1972-01-25 Thomas O Paine Spacecraft attitude control method and apparatus
US4012018A (en) * 1973-10-04 1977-03-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration All sky pointing attitude control system
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4193570A (en) * 1978-04-19 1980-03-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Active nutation controller
US4275861A (en) * 1978-08-04 1981-06-30 Rca Corporation Orientation of momentum stabilized vehicles
US4230294A (en) * 1979-07-23 1980-10-28 Rca Corporation Closed loop roll control for momentum biased satellites
US4618112A (en) * 1983-04-15 1986-10-21 Rca Corporation Spacecraft angular momentum stabilization system and method
US4961551A (en) * 1988-11-18 1990-10-09 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitary shape
US5012992A (en) * 1988-12-09 1991-05-07 Hughes Aircraft Company Spin stabilization via momentum wheels or similar devices
US5067673A (en) * 1990-02-07 1991-11-26 Hughes Aircraft Company Essentially passive method for inverting the orientation of a dual spin spacecraft
US5255878A (en) * 1990-08-03 1993-10-26 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
US5308024A (en) * 1992-07-20 1994-05-03 General Electric Co. Disturbance torque compensated three axis yaw control system
US5476239A (en) * 1994-04-19 1995-12-19 The United States Of America As Represented By The Secretary Of The Navy Gyro platform assembly with a spinning vehicle

Also Published As

Publication number Publication date
US5667171A (en) 1997-09-16
EP0739818A1 (de) 1996-10-30
EP0739818B1 (de) 1999-06-09
US5758846A (en) 1998-06-02
US6382565B1 (en) 2002-05-07
BR9602020A (pt) 1998-10-06
DE69602798D1 (de) 1999-07-15

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