FR2821683B1 - Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace - Google Patents

Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace

Info

Publication number
FR2821683B1
FR2821683B1 FR0102796A FR0102796A FR2821683B1 FR 2821683 B1 FR2821683 B1 FR 2821683B1 FR 0102796 A FR0102796 A FR 0102796A FR 0102796 A FR0102796 A FR 0102796A FR 2821683 B1 FR2821683 B1 FR 2821683B1
Authority
FR
France
Prior art keywords
stabilizing
orientation
controlling
space
machine
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
FR0102796A
Other languages
English (en)
Other versions
FR2821683A1 (fr
Inventor
Francis Vandenbussche
Michel Philippe Janvier
Overbeek Antonius Josephus Van
Antony Philip Holt
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.)
Agence Spatiale Europeenne
Original Assignee
Agence Spatiale Europeenne
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 Agence Spatiale Europeenne filed Critical Agence Spatiale Europeenne
Priority to FR0102796A priority Critical patent/FR2821683B1/fr
Priority to US10/084,270 priority patent/US6536713B2/en
Publication of FR2821683A1 publication Critical patent/FR2821683A1/fr
Application granted granted Critical
Publication of FR2821683B1 publication Critical patent/FR2821683B1/fr
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
    • 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
    • B64G1/244—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
    • B64G1/36—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Driving Devices And Active Controlling Of Vehicle (AREA)
FR0102796A 2001-03-01 2001-03-01 Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace Expired - Fee Related FR2821683B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0102796A FR2821683B1 (fr) 2001-03-01 2001-03-01 Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace
US10/084,270 US6536713B2 (en) 2001-03-01 2002-02-27 Method of controlling or stabilizing the attitude of a vehicle in space

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0102796A FR2821683B1 (fr) 2001-03-01 2001-03-01 Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace

Publications (2)

Publication Number Publication Date
FR2821683A1 FR2821683A1 (fr) 2002-09-06
FR2821683B1 true FR2821683B1 (fr) 2003-06-13

Family

ID=8860606

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0102796A Expired - Fee Related FR2821683B1 (fr) 2001-03-01 2001-03-01 Procede de commande pour controler ou stabiliser l'orientation d'un engin dans l'espace

Country Status (2)

Country Link
US (1) US6536713B2 (fr)
FR (1) FR2821683B1 (fr)

Families Citing this family (4)

* 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
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
US8380370B2 (en) * 2009-02-03 2013-02-19 The Boeing Company Spacecraft acquisition maneuvers using position-based gyroless control
FR2975180B1 (fr) * 2011-05-09 2019-05-31 Airbus Defence And Space Sas Dispositif et procede de determination d'attitude d'un satellite et satellite embarquant un tel dispositif.

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5123617A (en) * 1990-03-05 1992-06-23 General Electric Company Spacecraft momentum unloading using controlled magnetic torques
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.
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
US5201833A (en) * 1991-07-19 1993-04-13 General Electric Company Attitude control system with reaction wheel friction compensation
US5308024A (en) * 1992-07-20 1994-05-03 General Electric Co. Disturbance torque compensated three axis yaw control system
US5754023A (en) * 1995-10-26 1998-05-19 Cybernet Systems Corporation Gyro-stabilized platforms for force-feedback applications
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels
US6020956A (en) * 1999-02-04 2000-02-01 The Aerospace Corporation Pseudo gyro
US6298289B1 (en) * 1999-04-24 2001-10-02 The Boeing Company Integrated spacecraft control system and method
US6456907B1 (en) * 2000-01-31 2002-09-24 Space Systems/Loral, Inc. System and method for limiting the effects of actuator saturation to certain body axes of a spacecraft

Also Published As

Publication number Publication date
US6536713B2 (en) 2003-03-25
FR2821683A1 (fr) 2002-09-06
US20020121573A1 (en) 2002-09-05

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20151130