DE60304808T2 - Methode und Vorrichtung zur Lageregelung mit Solardruckmomenten während einer länger dauernden Entfaltung eines grossen Reflektors - Google Patents

Methode und Vorrichtung zur Lageregelung mit Solardruckmomenten während einer länger dauernden Entfaltung eines grossen Reflektors Download PDF

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Publication number
DE60304808T2
DE60304808T2 DE60304808T DE60304808T DE60304808T2 DE 60304808 T2 DE60304808 T2 DE 60304808T2 DE 60304808 T DE60304808 T DE 60304808T DE 60304808 T DE60304808 T DE 60304808T DE 60304808 T2 DE60304808 T2 DE 60304808T2
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Germany
Prior art keywords
spacecraft
solar
accessory
pulse
torque
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Expired - Lifetime
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DE60304808T
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German (de)
English (en)
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DE60304808D1 (de
Inventor
Hanching Grant Hacienda Heights Wang
Richard A. Rolling Hills Estates Fowell
Che-Hang C. Rancho Palos Verdes Ih
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Boeing Co
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Boeing Co
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Publication of DE60304808T2 publication Critical patent/DE60304808T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing
    • 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
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • 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
    • B64G1/242—Orbits and trajectories
    • 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
    • B64G1/32—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
    • 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
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443—Photovoltaic cell arrays
    • 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
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
DE60304808T 2002-12-13 2003-12-11 Methode und Vorrichtung zur Lageregelung mit Solardruckmomenten während einer länger dauernden Entfaltung eines grossen Reflektors Expired - Lifetime DE60304808T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US318715 2002-12-13
US10/318,715 US7025307B2 (en) 2002-12-13 2002-12-13 Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector

Publications (2)

Publication Number Publication Date
DE60304808D1 DE60304808D1 (de) 2006-06-01
DE60304808T2 true DE60304808T2 (de) 2006-12-21

Family

ID=32325974

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60304808T Expired - Lifetime DE60304808T2 (de) 2002-12-13 2003-12-11 Methode und Vorrichtung zur Lageregelung mit Solardruckmomenten während einer länger dauernden Entfaltung eines grossen Reflektors

Country Status (4)

Country Link
US (1) US7025307B2 (enExample)
EP (1) EP1428755B1 (enExample)
JP (1) JP4969019B2 (enExample)
DE (1) DE60304808T2 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102012490A (zh) * 2009-09-08 2011-04-13 上海卫星工程研究所 一种星载磁强计的安装布局

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7185858B2 (en) * 2003-11-26 2007-03-06 The Boeing Company Spacecraft gyro calibration system
US7762495B2 (en) * 2007-07-25 2010-07-27 The Boeing Company Solar powered aerial vehicle
US8386099B2 (en) * 2010-02-05 2013-02-26 Applied Defense Solutions Method and apparatus for initial orbit determination using high-precision orbit propagation and maneuver modeling
US20120158362A1 (en) * 2010-12-17 2012-06-21 Greenvolts, Inc. Remote angle mapping process for a cpv array
US9665453B2 (en) * 2012-09-12 2017-05-30 Honeywell International Inc. Launch vehicle testing system
CN103226019B (zh) * 2013-04-28 2015-07-08 北京控制工程研究所 一种用于双扫描红外地球敏感器的扫描镜组件
RU2580593C2 (ru) * 2014-06-10 2016-04-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ разгрузки силовых гироскопов космического аппарата с создаваемым магнитным моментом
US9764858B2 (en) * 2015-01-07 2017-09-19 Mitsubishi Electric Research Laboratories, Inc. Model predictive control of spacecraft
US9963248B2 (en) 2016-02-04 2018-05-08 The Boeing Company Spin stabilization of a spacecraft for an orbit maneuver
US11535406B2 (en) 2018-12-18 2022-12-27 The Boeing Company Satellites having autonomously deployable solar arrays
US11319093B2 (en) * 2019-05-06 2022-05-03 Eagle Technology, Llc Deployment mechanism for reflector antenna system
IT201900019322A1 (it) * 2019-10-18 2021-04-18 Thales Alenia Space Italia Spa Con Unico Socio Assistenza end-to-end in orbita
US20230399847A1 (en) * 2020-11-17 2023-12-14 L'garde, Inc. Light Weight, Low Stowed Volume, Space Deployable Batten-less Truss
CN115791050A (zh) * 2022-11-09 2023-03-14 北京工业大学 一种含均布陀螺桁架结构的实验装置
CN115817856B (zh) * 2022-11-21 2023-06-20 清华大学 基于纯磁控方式的卫星对日自旋稳定姿态控制方法及装置
CN116185721B (zh) * 2023-03-24 2023-09-08 北京控制工程研究所 卫星能源安全的保障方法、装置、计算设备及存储介质
CN120014815B (zh) * 2025-01-09 2025-09-23 中国科学院国家空间科学中心 一种探空火箭地面遥测系统设计方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4325124A (en) * 1979-02-28 1982-04-13 Organisation Europeenne De Recherches Spatiales System for controlling the direction of the momentum vector of a geosynchronous satellite
US4306692A (en) * 1979-03-16 1981-12-22 Communications Satellite Corporation Attitude acquisition maneuver for a bias momentum spacecraft
DE3329955A1 (de) * 1983-08-19 1985-03-07 Erno Raumfahrttechnik Gmbh, 2800 Bremen Lageregelung von satelliten
JPS63125498A (ja) * 1986-11-14 1988-05-28 三菱電機株式会社 人工衛星の姿勢制御装置
JPH01275300A (ja) * 1988-04-28 1989-11-02 Nec Corp 太陽輻射圧による宇宙飛翔体の姿勢制御法
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
US6017000A (en) * 1998-08-02 2000-01-25 Scott; David R. Apparatus and methods for in-space satellite operations
JP3366095B2 (ja) * 1994-02-10 2003-01-14 宇宙開発事業団 人工衛星の外乱トルク推定装置
US5816540A (en) 1995-12-22 1998-10-06 Hughes Electronics Optimal solar tracking system
US5906339A (en) * 1996-11-07 1999-05-25 Motorola, Inc. Multiple axis solar sailing
US6032903A (en) * 1998-02-12 2000-03-07 Hughes Electronics Corporation Cooperative control structures and methods for satellite spin axis control
US6138953A (en) * 1998-03-02 2000-10-31 Hughes Electronics Corporation Slew rate direction determination for acquisition maneuvers using reaction wheels
US6076773A (en) * 1998-04-10 2000-06-20 Hughes Electronics Corporation Spin-stabilized spacecraft and methods
US6463365B1 (en) * 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102012490A (zh) * 2009-09-08 2011-04-13 上海卫星工程研究所 一种星载磁强计的安装布局
CN102012490B (zh) * 2009-09-08 2013-05-22 上海卫星工程研究所 一种星载磁强计的支架结构

Also Published As

Publication number Publication date
US20040113020A1 (en) 2004-06-17
JP4969019B2 (ja) 2012-07-04
DE60304808D1 (de) 2006-06-01
US7025307B2 (en) 2006-04-11
EP1428755B1 (en) 2006-04-26
JP2004196289A (ja) 2004-07-15
EP1428755A1 (en) 2004-06-16

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