JPH04228400A - 極星センサを使用した宇宙船の３軸姿勢制御システム - Google Patents

極星センサを使用した宇宙船の３軸姿勢制御システム

Info

Publication number
JPH04228400A
JPH04228400A JP3109535A JP10953591A JPH04228400A JP H04228400 A JPH04228400 A JP H04228400A JP 3109535 A JP3109535 A JP 3109535A JP 10953591 A JP10953591 A JP 10953591A JP H04228400 A JPH04228400 A JP H04228400A
Authority
JP
Japan
Prior art keywords
signal
spacecraft
roll
pitch
star
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.)
Withdrawn
Application number
JP3109535A
Other languages
English (en)
Japanese (ja)
Inventor
Michael A Paluszek
マイケル・アダム・パルスゼック
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.)
General Electric Co
Original Assignee
General Electric 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 General Electric Co filed Critical General Electric Co
Publication of JPH04228400A publication Critical patent/JPH04228400A/ja
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/02—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means
    • 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
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782—Systems for determining direction or deviation from predetermined direction
    • G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
    • G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
    • G01S3/7867—Star trackers

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • General Physics & Mathematics (AREA)
  • Geology (AREA)
  • Geochemistry & Mineralogy (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP3109535A 1990-04-19 1991-04-16 極星センサを使用した宇宙船の３軸姿勢制御システム Withdrawn JPH04228400A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/511,169 US5107434A (en) 1990-04-19 1990-04-19 Three-axis spacecraft attitude control using polar star sensor
US511169 1995-08-04

Publications (1)

Publication Number Publication Date
JPH04228400A true JPH04228400A (ja) 1992-08-18

Family

ID=24033738

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3109535A Withdrawn JPH04228400A (ja) 1990-04-19 1991-04-16 極星センサを使用した宇宙船の３軸姿勢制御システム

Country Status (4)

Country Link
US (1) US5107434A (US06521211-20030218-C00004.png)
JP (1) JPH04228400A (US06521211-20030218-C00004.png)
DE (1) DE4112361A1 (US06521211-20030218-C00004.png)
FR (1) FR2661261A1 (US06521211-20030218-C00004.png)

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DE19703629A1 (de) * 1997-01-31 1998-08-06 Daimler Benz Aerospace Ag Verfahren zur bordautonomen Bestimmung der Position eines Satelliten
FR2666561B1 (fr) * 1990-09-06 1995-06-09 Aerospatiale Procede de pilotage d'un engin spatial dote d'un mouvement de precession et dispositif pour sa mise en óoeuvre.
FR2691426B1 (fr) * 1992-05-19 1997-09-19 Aerospatiale Procede et dispositif d'acquisition de la terre via la polaire pour satellite stabilise 3-axes en orbite de faible inclinaison.
US5348255A (en) * 1992-06-02 1994-09-20 Hughes Aircraft Company System and method for sensing attitude of a spacecraft with equilized star tracker errors along three orthogonal axes
US5608634A (en) * 1992-06-12 1997-03-04 Martin Marietta Corp. Low noise spacecraft body rate sensing arrangement for attitude control
US5319969A (en) * 1992-09-21 1994-06-14 Honeywell Inc. Method for determining 3-axis spacecraft attitude
US5319968A (en) * 1992-09-21 1994-06-14 Honeywell Inc. Apparatus for determining 3-axis space craft attitude
US5412574A (en) * 1993-05-14 1995-05-02 Hughes Aircraft Company Method of attitude determination using earth and star sensors
US5852792A (en) * 1996-10-03 1998-12-22 Lockheed Martin Corporation Spacecraft boresight calibration filter
US6216983B1 (en) * 1999-06-29 2001-04-17 Trw Inc. Ephemeris/attitude reference determination using communications links
US6142423A (en) * 1999-06-29 2000-11-07 Trw Inc. Ephemeris/attitude reference determination using on-board optics and other satellite ephemeris
US6360996B1 (en) * 2000-02-24 2002-03-26 Hughes Electronics Corporation Steering control for skewed scissors pair CMG clusters
AU2002251827A1 (en) 2001-01-26 2002-08-06 The Charles Stark Draper Laboratory, Inc. Miniature attitude sensing suite
US7878429B2 (en) * 2007-09-28 2011-02-01 Lindsay Corporation Solar powered irrigation machine
FR2922659B1 (fr) * 2007-10-19 2011-02-11 Thales Sa Systeme de visee absolue amelioree par combinaison d'un senseur d'etoiles et d'un capteur metrologique optique de vol en formation
US8218013B1 (en) * 2008-05-27 2012-07-10 Exelis, Inc Star sensing for an earth imaging sensor
US8222582B1 (en) * 2008-09-30 2012-07-17 Anderson Mark J Celestial navigation using stellar narrow-band emission
US8433515B2 (en) * 2011-07-06 2013-04-30 Tsinghua University Method for measuring precision of star sensor and system using the same
CN103344872B (zh) * 2013-06-28 2015-11-18 上海新跃仪表厂 一种星敏安装极性的测试方法
CN103323031B (zh) * 2013-06-28 2015-11-18 上海新跃仪表厂 一种基于星敏的地平仪系统误差在线补偿的方法
EP2879011B1 (en) * 2013-12-02 2021-02-03 Airbus Defence and Space GmbH On-board estimation of the nadir attitude of an Earth orbiting spacecraft
CN104833359B (zh) * 2015-05-27 2016-06-15 北京航空航天大学 一种基于离散马尔科夫特征序列模型的星图模式识别方法
CN106382927B (zh) * 2016-08-19 2019-10-18 哈尔滨工业大学 一种基于卫星识别的星敏感器自主导航方法
CN107121707B (zh) * 2017-05-09 2018-12-25 深圳清华大学研究院 一种三轴磁传感器测量基准与结构基准的误差校正方法
US10538342B2 (en) 2017-05-23 2020-01-21 Space Systems/Loral, Llc Ecliptic sun acquisition control mode for satellites
CN108364279B (zh) * 2017-12-26 2020-06-05 中国人民解放军战略支援部队信息工程大学 确定静止轨道遥感卫星指向偏差的方法
CN112093080B (zh) * 2020-09-22 2022-06-24 上海航天控制技术研究所 倾斜轨道卫星平台控制方法、电子设备及存储介质

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4114841A (en) * 1977-02-22 1978-09-19 Rca Corporation Magnetic torquing system for changing the spin rate of an orbiting satellite
FR2532911B1 (fr) * 1982-09-09 1986-06-27 Centre Nat Etd Spatiales Procede pour la correction d'orbite d'un satellite artificiel et dispositif correspondant
US4617634A (en) * 1983-06-28 1986-10-14 Mitsubishi Denki Kabushiki Kaisha Artificial satellite attitude control system
JPS60104499A (ja) * 1983-11-11 1985-06-08 株式会社日立製作所 姿勢決定方式
DE3428741A1 (de) * 1984-08-03 1986-02-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Messvorrichtung zur lagebestimmung fuer einen satelliten
JPS6171300A (ja) * 1984-09-13 1986-04-12 三菱電機株式会社 人工衛星の姿勢角計算装置
US4837699A (en) * 1985-07-18 1989-06-06 Hughes Aircraft Company Method for controlling the spin axis attitude of a spinning spacecraft
US4746976A (en) * 1986-05-23 1988-05-24 Ford Aerospace & Communications Corporation Star sightings by satellite for image navigation
US4827422A (en) * 1986-12-04 1989-05-02 Barnes Engineering Company Fan scan horizon sensor for a spin stabilized satellite
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system
USH712H (en) * 1988-08-03 1989-11-07 The United States Of America As Represented By The Secretary Of The Army Method of stellar navigation using an optical correlator
FR2637564B1 (fr) * 1988-10-06 1994-10-14 Aerospatiale Procede et systeme de controle autonome d'orbite d'un satellite geostationnaire
US5012081A (en) * 1989-06-22 1991-04-30 Northrop Corporation Strapdown stellar sensor and holographic lens therefor

Also Published As

Publication number Publication date
FR2661261B1 (US06521211-20030218-C00004.png) 1995-01-20
FR2661261A1 (fr) 1991-10-25
US5107434A (en) 1992-04-21
DE4112361A1 (de) 1991-10-24

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Legal Events

Date Code Title Description
A300 Application deemed to be withdrawn because no request for examination was validly filed

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 19980711