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FR2981050B1 - Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile - Google Patents

Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile

Info

Publication number
FR2981050B1
FR2981050B1 FR1103064A FR1103064A FR2981050B1 FR 2981050 B1 FR2981050 B1 FR 2981050B1 FR 1103064 A FR1103064 A FR 1103064A FR 1103064 A FR1103064 A FR 1103064A FR 2981050 B1 FR2981050 B1 FR 2981050B1
Authority
FR
France
Prior art keywords
actuator control
satellite attitude
agile satellite
gyroscopic actuator
direct formulation
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.)
Active
Application number
FR1103064A
Other languages
English (en)
Other versions
FR2981050A1 (fr
Inventor
Larminat Philippe De
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR1103064A priority Critical patent/FR2981050B1/fr
Publication of FR2981050A1 publication Critical patent/FR2981050A1/fr
Application granted granted Critical
Publication of FR2981050B1 publication Critical patent/FR2981050B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244Spacecraft control systems

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)
FR1103064A 2011-10-07 2011-10-07 Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile Active FR2981050B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1103064A FR2981050B1 (fr) 2011-10-07 2011-10-07 Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1103064A FR2981050B1 (fr) 2011-10-07 2011-10-07 Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile

Publications (2)

Publication Number Publication Date
FR2981050A1 FR2981050A1 (fr) 2013-04-12
FR2981050B1 true FR2981050B1 (fr) 2014-07-25

Family

ID=45688542

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1103064A Active FR2981050B1 (fr) 2011-10-07 2011-10-07 Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile

Country Status (1)

Country Link
FR (1) FR2981050B1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6154691A (en) * 1997-09-02 2000-11-28 Honeywell International Inc. Orienting a satellite with controlled momentum gyros
FR2786283B1 (fr) * 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
FR2826470B1 (fr) * 2001-06-26 2003-09-19 Astrium Sas Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes

Also Published As

Publication number Publication date
FR2981050A1 (fr) 2013-04-12

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