DE69721346D1 - Dynamische Momenten-Vorsteuerung für die Gierregelung im Weltraum - Google Patents

Dynamische Momenten-Vorsteuerung für die Gierregelung im Weltraum

Info

Publication number
DE69721346D1
DE69721346D1 DE69721346T DE69721346T DE69721346D1 DE 69721346 D1 DE69721346 D1 DE 69721346D1 DE 69721346 T DE69721346 T DE 69721346T DE 69721346 T DE69721346 T DE 69721346T DE 69721346 D1 DE69721346 D1 DE 69721346D1
Authority
DE
Germany
Prior art keywords
control
space
dynamic torque
yaw
torque pilot
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
DE69721346T
Other languages
English (en)
Inventor
John J Rodden
Walter Fichter
Nobuo Furumoto
Ernst Bruederle
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 Defence and Space GmbH
Globalstar LP
Original Assignee
DaimlerChrysler Aerospace AG
Globalstar LP
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 Aerospace AG, Globalstar LP filed Critical DaimlerChrysler Aerospace AG
Application granted granted Critical
Publication of DE69721346D1 publication Critical patent/DE69721346D1/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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers
    • 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
    • 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
    • B64G1/24—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)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
DE69721346T 1996-01-16 1997-01-08 Dynamische Momenten-Vorsteuerung für die Gierregelung im Weltraum Expired - Lifetime DE69721346D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/585,954 US5791598A (en) 1996-01-16 1996-01-16 Dynamic bias for orbital yaw steering

Publications (1)

Publication Number Publication Date
DE69721346D1 true DE69721346D1 (de) 2003-06-05

Family

ID=24343693

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69721346T Expired - Lifetime DE69721346D1 (de) 1996-01-16 1997-01-08 Dynamische Momenten-Vorsteuerung für die Gierregelung im Weltraum

Country Status (8)

Country Link
US (1) US5791598A (de)
EP (1) EP0785132B1 (de)
JP (1) JPH09325045A (de)
KR (1) KR970059710A (de)
CN (1) CN1174982A (de)
BR (1) BR9700052A (de)
CA (1) CA2194252A1 (de)
DE (1) DE69721346D1 (de)

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US6704607B2 (en) 2001-05-21 2004-03-09 The Boeing Company Method and apparatus for controllably positioning a solar concentrator
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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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CN100363851C (zh) * 2004-11-26 2008-01-23 清华大学 航天器大角度机动控制的单框架力矩陀螺群的最优控制法
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CN102050228B (zh) * 2010-10-11 2013-06-19 北京控制工程研究所 一种利用陀螺和喷气时间联合诊断喷管堵塞故障的方法
RU2467929C2 (ru) * 2010-12-13 2012-11-27 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ построения орбитальной ориентации пилотируемого космического аппарата
CN102163057B (zh) * 2011-04-14 2013-05-29 北京航空航天大学 一种自治飞艇平面路径跟踪控制方法
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CN102320378B (zh) * 2011-06-20 2013-07-24 北京航空航天大学 多操纵面飞机的一种均衡操纵分配方法
CN102514734B (zh) * 2011-10-27 2013-11-27 北京航空航天大学 基于日地系统Halo轨道探测器构型与姿态指向的姿态递推方法
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CN103171775B (zh) * 2013-01-30 2015-03-18 北京控制工程研究所 一种基于轨控干扰的角动量耦合卸载方法
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CN106326576B (zh) * 2016-08-26 2019-07-12 北京控制工程研究所 一种任意基准系下的整星偏置角动量的偏航估计方法
CN106354146B (zh) * 2016-10-31 2023-05-05 榆林学院 一种串联式姿态控制平台及控制方法
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CN106586034A (zh) * 2016-12-20 2017-04-26 上海微小卫星工程中心 卫星旋转部件动静不平衡干扰力矩自补偿方法
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Also Published As

Publication number Publication date
BR9700052A (pt) 1998-11-10
CA2194252A1 (en) 1997-07-17
US5791598A (en) 1998-08-11
EP0785132A1 (de) 1997-07-23
EP0785132B1 (de) 2003-05-02
CN1174982A (zh) 1998-03-04
JPH09325045A (ja) 1997-12-16
KR970059710A (ko) 1997-08-12

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