ATE286830T1 - Methode und vorrichtung zur bestimmung des gierwinkels eines satelliten - Google Patents

Methode und vorrichtung zur bestimmung des gierwinkels eines satelliten

Info

Publication number
ATE286830T1
ATE286830T1 AT99971773T AT99971773T ATE286830T1 AT E286830 T1 ATE286830 T1 AT E286830T1 AT 99971773 T AT99971773 T AT 99971773T AT 99971773 T AT99971773 T AT 99971773T AT E286830 T1 ATE286830 T1 AT E286830T1
Authority
AT
Austria
Prior art keywords
satellite
determining
yaw angle
yaw
angle
Prior art date
Application number
AT99971773T
Other languages
English (en)
Inventor
Christian Patouraux
Original Assignee
Ses Astra Sa
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 Ses Astra Sa filed Critical Ses Astra Sa
Application granted granted Critical
Publication of ATE286830T1 publication Critical patent/ATE286830T1/de

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
    • G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • 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
    • B64G1/285—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
    • 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
    • B64G1/24—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT99971773T 1998-11-06 1999-11-08 Methode und vorrichtung zur bestimmung des gierwinkels eines satelliten ATE286830T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP98120693A EP0999128A1 (de) 1998-11-06 1998-11-06 Methode zur Bestimmung des Gierwinkels eines Satelliten
PCT/EP1999/008546 WO2000027701A1 (en) 1998-11-06 1999-11-08 Method and apparatus for determining the yaw angle of a satellite

Publications (1)

Publication Number Publication Date
ATE286830T1 true ATE286830T1 (de) 2005-01-15

Family

ID=8232899

Family Applications (1)

Application Number Title Priority Date Filing Date
AT99971773T ATE286830T1 (de) 1998-11-06 1999-11-08 Methode und vorrichtung zur bestimmung des gierwinkels eines satelliten

Country Status (8)

Country Link
US (1) US6804986B2 (de)
EP (2) EP0999128A1 (de)
AR (1) AR023698A1 (de)
AT (1) ATE286830T1 (de)
AU (1) AU1381200A (de)
BR (1) BR9915075A (de)
DE (1) DE69923209D1 (de)
WO (1) WO2000027701A1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0213485D0 (en) 2002-06-12 2002-07-24 Bp Chem Int Ltd Process
US6762716B2 (en) * 2002-12-13 2004-07-13 The Boeing Company Digital beacon asymmetry and quantization compensation
US7185858B2 (en) * 2003-11-26 2007-03-06 The Boeing Company Spacecraft gyro calibration system
RU2256154C1 (ru) * 2004-06-16 2005-07-10 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" (ОАО МНПК "Авионика") Способ измерения угловых положений летательного аппарата
KR20070073273A (ko) * 2006-01-04 2007-07-10 삼성전자주식회사 휴대용 단말기에서 폴더의 회전 상태를 감지하는 장치 및방법
CN102410842B (zh) * 2011-07-26 2013-05-08 西安费斯达自动化工程有限公司 基于铅垂陀螺和ccd线阵的姿态可视化测量方法
US9091552B2 (en) 2011-10-25 2015-07-28 The Boeing Company Combined location and attitude determination system and methods
FR2995478B1 (fr) * 2012-09-07 2014-09-26 Thales Sa Methode pour la caracterisation d'une antenne de transmission d'un satellite en orbite et systeme associe
DE102014004060B4 (de) * 2014-03-10 2015-10-22 Northrop Grumman Litef Gmbh Verfahren und vorrichtung zum bestimmen von navigationsdaten
CN108958064B (zh) * 2017-05-17 2021-10-01 上海微小卫星工程中心 姿态导引律误差判断方法、系统及电子设备
CN111591472B (zh) * 2020-05-15 2021-12-10 北京世冠金洋科技发展有限公司 一种调整卫星姿态的方法和相关装置
CN119077754B (zh) * 2024-11-06 2025-03-18 哈尔滨思哲睿智能医疗设备股份有限公司 一种分体式机器人的标定方法、装置、设备、介质及产品

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4827422A (en) * 1986-12-04 1989-05-02 Barnes Engineering Company Fan scan horizon sensor for a spin stabilized satellite
US5257760A (en) * 1992-06-24 1993-11-02 Edo Corporation, Barnes Engineering Division Scanning earth sensor using the sun's position for determining yaw
US5319968A (en) * 1992-09-21 1994-06-14 Honeywell Inc. Apparatus for determining 3-axis space craft attitude
US5556058A (en) * 1994-05-16 1996-09-17 Hughes Electronics Spacecraft attitude determination using sun sensor, earth sensor, and space-to-ground link

Also Published As

Publication number Publication date
AR023698A1 (es) 2002-09-04
HK1037870A1 (en) 2002-02-22
BR9915075A (pt) 2001-07-17
DE69923209D1 (de) 2005-02-17
EP1127004B1 (de) 2005-01-12
US20020116993A1 (en) 2002-08-29
WO2000027701A1 (en) 2000-05-18
EP0999128A1 (de) 2000-05-10
EP1127004A1 (de) 2001-08-29
AU1381200A (en) 2000-05-29
US6804986B2 (en) 2004-10-19

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties