DE68926149D1 - Stabilisierung eines drallstabilisierten Raumfahrzeuges mit beliebiger Form - Google Patents

Stabilisierung eines drallstabilisierten Raumfahrzeuges mit beliebiger Form

Info

Publication number
DE68926149D1
DE68926149D1 DE68926149T DE68926149T DE68926149D1 DE 68926149 D1 DE68926149 D1 DE 68926149D1 DE 68926149 T DE68926149 T DE 68926149T DE 68926149 T DE68926149 T DE 68926149T DE 68926149 D1 DE68926149 D1 DE 68926149D1
Authority
DE
Germany
Prior art keywords
stabilization
spin
shape
stabilized spacecraft
spacecraft
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
DE68926149T
Other languages
English (en)
Other versions
DE68926149T2 (de
Inventor
Harold A Rosen
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 Aircraft Co
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 Aircraft Co filed Critical Hughes Aircraft Co
Publication of DE68926149D1 publication Critical patent/DE68926149D1/de
Application granted granted Critical
Publication of DE68926149T2 publication Critical patent/DE68926149T2/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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE68926149T 1988-11-18 1989-11-17 Stabilisierung eines drallstabilisierten Raumfahrzeuges mit beliebiger Form Expired - Lifetime DE68926149T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/272,858 US4961551A (en) 1988-11-18 1988-11-18 Stabilization of a spinning spacecraft of arbitary shape

Publications (2)

Publication Number Publication Date
DE68926149D1 true DE68926149D1 (de) 1996-05-09
DE68926149T2 DE68926149T2 (de) 1996-11-28

Family

ID=23041609

Family Applications (1)

Application Number Title Priority Date Filing Date
DE68926149T Expired - Lifetime DE68926149T2 (de) 1988-11-18 1989-11-17 Stabilisierung eines drallstabilisierten Raumfahrzeuges mit beliebiger Form

Country Status (6)

Country Link
US (1) US4961551A (de)
EP (1) EP0371344B1 (de)
JP (1) JP2536939B2 (de)
AU (1) AU610765B2 (de)
CA (1) CA2000675C (de)
DE (1) DE68926149T2 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0445011B1 (de) * 1990-02-26 1993-11-10 AEROSPATIALE Société Nationale Industrielle Geostationärer Beobachtungssatellit mit einem mehrdüsigen flüssigtreibstoffgetriebenen Apogäumsmanövriersystem
US5098041A (en) * 1990-06-07 1992-03-24 Hughes Aircraft Company Attitude control system for momentum-biased spacecraft
US5130931A (en) * 1990-07-13 1992-07-14 General Electric Company Spacecraft attitude and velocity control system
US5140525A (en) * 1991-07-31 1992-08-18 General Electric Company Unified spacecraft attitude control system
US5311435A (en) * 1991-11-27 1994-05-10 Hughes Aircraft Company Method for station keeping control of flexible spacecraft using onboard gain scheduling scheme
CA2076894C (en) * 1991-11-27 1998-11-03 John F. Yocum Three axis thruster modulation
US5308025A (en) * 1992-07-30 1994-05-03 Hughes Aircraft Company Spacecraft spin axis capture system and method
US5562266A (en) * 1992-10-29 1996-10-08 Aerospatiale Societe Nationale Industrielle Rate gyro calibration method and apparatus for a three-axis stabilized satellite
FR2697651B1 (fr) * 1992-10-29 1995-02-03 Aerospatiale Procédé et appareil de calibration des gyromètres d'un satellite stabilisé 3-axes.
US5452869A (en) * 1992-12-18 1995-09-26 Hughes Aircraft Company On-board three-axes attitude determination and control system
US5411227A (en) * 1992-12-23 1995-05-02 Hughes Aircraft Company Satellite thruster uncertainty estimation in transition mode
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
US5395076A (en) * 1993-03-19 1995-03-07 Martin Marietta Corporation Spacecraft velocity change maneuvers by variable arcjets
US5667171A (en) * 1995-04-28 1997-09-16 Hughes Aircraft Company Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device
DE19519732A1 (de) * 1995-06-02 1996-12-05 Daimler Benz Aerospace Ag Düsenanordnung und Verfahren zur Ansteuerung der Düsen
US5646847A (en) * 1995-08-25 1997-07-08 Martin Marietta Corp. Universal thruster selection logic for spacecraft attitude control
US5850993A (en) * 1995-08-25 1998-12-22 Martin Marietta Corp. Spacecraft thruster operation for improved orbital maneuver accuracy
US6102337A (en) * 1995-12-22 2000-08-15 Hughes Electronics Corporation Spacecraft attitude control with gimbaled thrusters
JP3867315B2 (ja) * 1996-04-22 2007-01-10 三菱電機株式会社 自動衝突回避装置
US6052630A (en) * 1996-12-17 2000-04-18 Space Systems/Loral, Inc. Thruster optimized pair selection
US6125310A (en) * 1997-07-18 2000-09-26 Space Systems/Loral, Inc. Thruster on time signaling with flexure compensation avoidance
US6032903A (en) * 1998-02-12 2000-03-07 Hughes Electronics Corporation Cooperative control structures and methods for satellite spin axis control
US6076773A (en) * 1998-04-10 2000-06-20 Hughes Electronics Corporation Spin-stabilized spacecraft and methods
US7173285B2 (en) * 2004-03-18 2007-02-06 Cree, Inc. Lithographic methods to reduce stacking fault nucleation sites
US7302317B2 (en) * 2004-04-29 2007-11-27 The Boeing Company System and method to enhance attitude estimation for transfer orbit maneuver
CN103303496B (zh) * 2013-06-28 2015-09-09 上海新跃仪表厂 一种微幅调整轨道高度的方法
US10435087B2 (en) 2017-03-21 2019-10-08 Kenneth Hardin Personal transportation vehicle
CN109649692B (zh) * 2018-12-28 2021-10-01 上海航天控制技术研究所 一种基于推力器偏差估计的轨控策略在轨修正方法和系统

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2373823A1 (fr) * 1976-12-10 1978-07-07 Matra Procede et dispositif de commande d'attitude de vehicule spatial
US4386750A (en) * 1980-08-29 1983-06-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of damping nutation motion with minimum spin axis attitude disturbance
DE3212574A1 (de) * 1982-04-03 1983-10-20 Dornier System Gmbh, 7990 Friedrichshafen Verfahren zur lageaenderung eines satelliten
US4599697A (en) * 1982-08-11 1986-07-08 Ford Aerospace & Communications Corporation Digital PWPF three axis spacecraft attitude control
US4725024A (en) * 1985-11-15 1988-02-16 Ford Aerospace & Communications Corporation Method for spinning up a three-axis controlled spacecraft
US4767084A (en) * 1986-09-18 1988-08-30 Ford Aerospace & Communications Corporation Autonomous stationkeeping for three-axis stabilized spacecraft

Also Published As

Publication number Publication date
JP2536939B2 (ja) 1996-09-25
EP0371344A3 (de) 1991-08-07
EP0371344B1 (de) 1996-04-03
CA2000675C (en) 1994-10-25
AU4531189A (en) 1990-05-24
US4961551A (en) 1990-10-09
EP0371344A2 (de) 1990-06-06
JPH02179600A (ja) 1990-07-12
DE68926149T2 (de) 1996-11-28
CA2000675A1 (en) 1990-05-18
AU610765B2 (en) 1991-05-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: HUGHES ELECTRONICS CORP., EL SEGUNDO, CALIF., US

8328 Change in the person/name/address of the agent

Representative=s name: WITTE, WELLER & PARTNER, 70178 STUTTGART