FR2759974B1 - METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE - Google Patents

METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE

Info

Publication number
FR2759974B1
FR2759974B1 FR9702088A FR9702088A FR2759974B1 FR 2759974 B1 FR2759974 B1 FR 2759974B1 FR 9702088 A FR9702088 A FR 9702088A FR 9702088 A FR9702088 A FR 9702088A FR 2759974 B1 FR2759974 B1 FR 2759974B1
Authority
FR
France
Prior art keywords
satellite
speed sensor
angular speed
inertial actuator
integrated inertial
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
FR9702088A
Other languages
French (fr)
Other versions
FR2759974A1 (en
Inventor
Philippe Laurens
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.)
Matra Marconi Space France SA
Original Assignee
Matra Marconi Space France 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 Matra Marconi Space France SA filed Critical Matra Marconi Space France SA
Priority to FR9702088A priority Critical patent/FR2759974B1/en
Publication of FR2759974A1 publication Critical patent/FR2759974A1/en
Application granted granted Critical
Publication of FR2759974B1 publication Critical patent/FR2759974B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/42—Rotary gyroscopes for indicating rate of turn; for integrating rate of turn
    • 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
    • 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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
FR9702088A 1997-02-21 1997-02-21 METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE Expired - Fee Related FR2759974B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9702088A FR2759974B1 (en) 1997-02-21 1997-02-21 METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9702088A FR2759974B1 (en) 1997-02-21 1997-02-21 METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE

Publications (2)

Publication Number Publication Date
FR2759974A1 FR2759974A1 (en) 1998-08-28
FR2759974B1 true FR2759974B1 (en) 1999-05-14

Family

ID=9504029

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9702088A Expired - Fee Related FR2759974B1 (en) 1997-02-21 1997-02-21 METHOD AND INTEGRATED INERTIAL ACTUATOR AND ANGULAR SPEED SENSOR OF A SATELLITE

Country Status (1)

Country Link
FR (1) FR2759974B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116176870B (en) * 2023-03-20 2023-09-19 北京星途探索科技有限公司 Solid attitude and orbit control power system for aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362229A (en) * 1964-01-23 1968-01-09 Gen Motors Corp Transverse angular velocity sensor
US3902374A (en) * 1973-10-19 1975-09-02 Singer Co Electrostatic rate gyroscope
US4061043A (en) * 1976-03-29 1977-12-06 John Callender Stiles Electrostatic rate gyroscope
US5112012A (en) * 1989-10-26 1992-05-12 Yuan Mark S Tilting momentum wheel for spacecraft
US5441222A (en) * 1993-04-26 1995-08-15 Hughes Aircraft Company Attitude control of spinning spacecraft

Also Published As

Publication number Publication date
FR2759974A1 (en) 1998-08-28

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Legal Events

Date Code Title Description
ST Notification of lapse