DE69606275T2 - Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges - Google Patents

Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges

Info

Publication number
DE69606275T2
DE69606275T2 DE69606275T DE69606275T DE69606275T2 DE 69606275 T2 DE69606275 T2 DE 69606275T2 DE 69606275 T DE69606275 T DE 69606275T DE 69606275 T DE69606275 T DE 69606275T DE 69606275 T2 DE69606275 T2 DE 69606275T2
Authority
DE
Germany
Prior art keywords
stabilized
earth
position control
inertia
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 - Fee Related
Application number
DE69606275T
Other languages
English (en)
Other versions
DE69606275D1 (de
Inventor
Michael Dipl Ing Surauer
Walter Dipl Ing Fichter
Ernst Dipl-Math Bruederle
Peter Dr Zentgraf
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.)
Airbus DS GmbH
Original Assignee
DaimlerChrysler AG
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 DaimlerChrysler AG filed Critical DaimlerChrysler AG
Publication of DE69606275D1 publication Critical patent/DE69606275D1/de
Application granted granted Critical
Publication of DE69606275T2 publication Critical patent/DE69606275T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • 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
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft 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
    • B64G1/28—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
    • B64G1/285—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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69606275T 1995-08-11 1996-08-12 Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges Expired - Fee Related DE69606275T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP95112723 1995-08-11

Publications (2)

Publication Number Publication Date
DE69606275D1 DE69606275D1 (de) 2000-02-24
DE69606275T2 true DE69606275T2 (de) 2000-07-13

Family

ID=8219520

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69606275T Expired - Fee Related DE69606275T2 (de) 1995-08-11 1996-08-12 Verfahren zur Lageregelung eines dreiachsenstabilisierten, erdorientierten trägheitsmomentstabilisierten Raumfahrzeuges

Country Status (2)

Country Link
US (1) US5996941A (de)
DE (1) DE69606275T2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10342866A1 (de) * 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung

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DE19816978C1 (de) * 1998-04-17 1999-11-04 Daimler Chrysler Ag Verfahren zur Identifizierung eines fehlerhaft messenden Sensors in einem Raumfahrzeug
US6145790A (en) * 1998-09-22 2000-11-14 Hughes Electronics Corporation Attitude determination system and method
DE19843774C1 (de) * 1998-09-24 1999-11-11 Deutsch Zentr Luft & Raumfahrt Raumfahrzeug
US6430393B1 (en) * 1999-08-23 2002-08-06 Hughes Electronics Corporation Satellite communication system using linear cell tracking
US6311932B1 (en) * 1999-11-30 2001-11-06 Space Systems/Loral Inc. Yaw steering momentum system
US6470243B1 (en) * 2000-06-30 2002-10-22 Hughes Electronics Corp. Correction of spacecraft steering control law for unexpected orbital inclination effects
AU2002251827A1 (en) 2001-01-26 2002-08-06 The Charles Stark Draper Laboratory, Inc. Miniature attitude sensing suite
US6928400B2 (en) * 2001-10-02 2005-08-09 Raytheon Company Method for designing a deployment mechanism
US6732977B1 (en) * 2002-02-11 2004-05-11 Lockheed Martin Corporation System for on-orbit correction of spacecraft payload pointing errors
US6695263B1 (en) 2002-02-12 2004-02-24 Lockheed Martin Corporation System for geosynchronous spacecraft rapid earth reacquisition
US7051980B2 (en) * 2002-02-26 2006-05-30 Lockheed Martin Corporation Efficient orbit sparing system for space vehicle constellations
US6702234B1 (en) 2002-03-29 2004-03-09 Lockheed Martin Corporation Fault tolerant attitude control system for zero momentum spacecraft
US7835826B1 (en) 2005-12-13 2010-11-16 Lockheed Martin Corporation Attitude determination system for yaw-steering spacecraft
CN100351144C (zh) * 2006-05-31 2007-11-28 哈尔滨工业大学 基于行为模式的深空三轴稳定姿态定向控制方法
RU2618856C1 (ru) * 2016-03-31 2017-05-11 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ управления пространственной ориентацией космического аппарата и система управления для его реализации
US11124320B2 (en) * 2019-02-12 2021-09-21 Canadian Space Agency Spacecraft control using residual dipole
DE102020206659A1 (de) * 2019-05-30 2020-12-03 Robert Bosch Gesellschaft mit beschränkter Haftung Multi-hypothesen-objektverfologung für automatisierte fahrsysteme
CN110808447A (zh) * 2019-10-24 2020-02-18 迪泰（浙江）通信技术有限公司 基于三轴动态跟踪技术的船载卫星天线系统
DE102020107172A1 (de) * 2020-03-16 2021-09-16 Volocopter Gmbh Verfahren zur Steuerung eines Fluggeräts, Steuerungseinrichtung für ein Fluggerät und Fluggerät mit einer solchen Steuerungseinrichtung
CN112684697B (zh) * 2020-12-15 2022-07-29 上海卫星工程研究所 分体式卫星在轨两舱转动惯量辨识方法及系统
CN113485095B (zh) * 2021-08-11 2022-09-13 中国科学院微小卫星创新研究院 北斗三号卫星处于地影期时预报姿态的方法
CN115327921A (zh) * 2022-09-01 2022-11-11 深圳航天东方红卫星有限公司 一种在轨航天器纯三轴磁控方法
CN116610137B (zh) * 2023-07-19 2023-09-15 北京航空航天大学 一种基于干扰预示的高超声速飞行器强抗扰控制方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5058835A (en) * 1990-06-11 1991-10-22 General Electric Company Wheel speed management control system for spacecraft
US5608634A (en) * 1992-06-12 1997-03-04 Martin Marietta Corp. Low noise spacecraft body rate sensing arrangement for attitude control
US5308024A (en) * 1992-07-20 1994-05-03 General Electric Co. Disturbance torque compensated three axis yaw control system
US5452869A (en) * 1992-12-18 1995-09-26 Hughes Aircraft Company On-board three-axes attitude determination and control system
DE4429536C2 (de) * 1994-08-19 1999-01-14 Man Takraf Foerdertechnik Gmbh Stetigfördernder Schiffsentlader

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10342866A1 (de) * 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung
US7797085B2 (en) 2003-09-15 2010-09-14 Astrium Gmbh Process for determining the position of a spacecraft with the aid of a directional vector and a total angular momentum measurement
US7996119B2 (en) 2003-09-15 2011-08-09 Astrium Gmbh Method for determining the position of a spacecraft with the aid of a direction vector and an overall spin measurement

Also Published As

Publication number Publication date
US5996941A (en) 1999-12-07
DE69606275D1 (de) 2000-02-24

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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: ASTRIUM GMBH, 81667 MUENCHEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: EADS ASTRIUM GMBH, 81667 MUENCHEN, DE

8339 Ceased/non-payment of the annual fee