FR2373823A1 - Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw - Google Patents

Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw

Info

Publication number
FR2373823A1
FR2373823A1 FR7637351A FR7637351A FR2373823A1 FR 2373823 A1 FR2373823 A1 FR 2373823A1 FR 7637351 A FR7637351 A FR 7637351A FR 7637351 A FR7637351 A FR 7637351A FR 2373823 A1 FR2373823 A1 FR 2373823A1
Authority
FR
France
Prior art keywords
yaw
roll
pitch
space vehicle
orbital trajectory
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.)
Granted
Application number
FR7637351A
Other languages
French (fr)
Other versions
FR2373823B1 (en
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.)
Societe des Telephones Ericsson SA
Original Assignee
Societe des Telephones Ericsson 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 Societe des Telephones Ericsson SA filed Critical Societe des Telephones Ericsson SA
Priority to FR7637351A priority Critical patent/FR2373823A1/en
Publication of FR2373823A1 publication Critical patent/FR2373823A1/en
Application granted granted Critical
Publication of FR2373823B1 publication Critical patent/FR2373823B1/fr
Granted 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
    • 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

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)

Abstract

A space vehicle on an orbital trajectory is controlled in attitude before ejection into a geostationary orbit. The control system controls in pitch yaw and roll w.r.t. an inertial attitude memory. An attitude control system comprises three integrating gyroscopes (14x, y, z) for roll pitch and yaw attitudes. The gyro outputs are filtered (17) and applied to logic threshold circuits (18) prior to application to control circuits (20) for thrust output tubes (19, 24, 25) which rotate the vehicle as required. A register (28) output control torque motors (26, 27) on roll and pitch gyros after reception of remote control signals which are received (29) and validated (30) in conjunction with output from a solar sensor (30).
FR7637351A 1976-12-10 1976-12-10 Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw Granted FR2373823A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7637351A FR2373823A1 (en) 1976-12-10 1976-12-10 Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7637351A FR2373823A1 (en) 1976-12-10 1976-12-10 Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw

Publications (2)

Publication Number Publication Date
FR2373823A1 true FR2373823A1 (en) 1978-07-07
FR2373823B1 FR2373823B1 (en) 1980-09-05

Family

ID=9180937

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7637351A Granted FR2373823A1 (en) 1976-12-10 1976-12-10 Space vehicle orbital trajectory control - is performed by integrating gyroscopes system w.r.t. inertial attitude memory for roll pitch and yaw

Country Status (1)

Country Link
FR (1) FR2373823A1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2447320A1 (en) * 1979-01-23 1980-08-22 Matra IMPROVEMENTS TO ACTIVE NUTATION DAMPING METHODS AND DEVICES FOR SPATIAL VEHICLE
FR2532911A1 (en) * 1982-09-09 1984-03-16 Centre Nat Etd Spatiales Method for orbital correction of an artificial satellite and corresponding device
FR2581966A1 (en) * 1985-05-17 1986-11-21 Rca Corp METHOD AND SYSTEM FOR STABILIZING A SPACE VEHICLE
FR2583873A1 (en) * 1985-06-20 1986-12-26 Matra METHOD AND DEVICE FOR INJECTING SATELLITE ONTO GEOSTATIONARY ORBIT WITH STABILIZATION FOLLOWING THE THREE AXES
EP0371344A2 (en) * 1988-11-18 1990-06-06 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitrary shape
EP0375496A1 (en) * 1988-12-23 1990-06-27 AEROSPATIALE Société Nationale Industrielle Attitude determination and control system for a spin-stabilized satellite in an elliptic transfer orbit
EP0394897A1 (en) * 1989-04-24 1990-10-31 Alcatel Espace Method for posting a geostationary telecommunication satellite
CN115290254A (en) * 2022-10-09 2022-11-04 中国西安卫星测控中心 On-orbit identification method for rotational inertia of combined spacecraft

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2447320A1 (en) * 1979-01-23 1980-08-22 Matra IMPROVEMENTS TO ACTIVE NUTATION DAMPING METHODS AND DEVICES FOR SPATIAL VEHICLE
FR2532911A1 (en) * 1982-09-09 1984-03-16 Centre Nat Etd Spatiales Method for orbital correction of an artificial satellite and corresponding device
FR2581966A1 (en) * 1985-05-17 1986-11-21 Rca Corp METHOD AND SYSTEM FOR STABILIZING A SPACE VEHICLE
FR2583873A1 (en) * 1985-06-20 1986-12-26 Matra METHOD AND DEVICE FOR INJECTING SATELLITE ONTO GEOSTATIONARY ORBIT WITH STABILIZATION FOLLOWING THE THREE AXES
EP0209429A1 (en) * 1985-06-20 1987-01-21 Matra Method and device for placing a 3-axis stabilized satellite into a geostationary orbit
JPH02179600A (en) * 1988-11-18 1990-07-12 Hughes Aircraft Co System of stabilizing space flying object rotating in optional geometry
EP0371344A2 (en) * 1988-11-18 1990-06-06 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitrary shape
EP0371344A3 (en) * 1988-11-18 1991-08-07 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitrary shape
EP0375496A1 (en) * 1988-12-23 1990-06-27 AEROSPATIALE Société Nationale Industrielle Attitude determination and control system for a spin-stabilized satellite in an elliptic transfer orbit
FR2640933A1 (en) * 1988-12-23 1990-06-29 Aerospatiale
US5064152A (en) * 1988-12-23 1991-11-12 Aerospatiale Societe Nationale Industrielle Method of determining and controlling the attitude of a spin-stabilized satellite in an elliptical transfer orbit
EP0394897A1 (en) * 1989-04-24 1990-10-31 Alcatel Espace Method for posting a geostationary telecommunication satellite
FR2647565A1 (en) * 1989-04-24 1990-11-30 Alcatel Espace METHOD FOR POSTING A GEOSTATIONARY TELECOMMUNICATIONS SATELLITE
CN115290254A (en) * 2022-10-09 2022-11-04 中国西安卫星测控中心 On-orbit identification method for rotational inertia of combined spacecraft
CN115290254B (en) * 2022-10-09 2023-02-03 中国西安卫星测控中心 On-orbit identification method for rotational inertia of combined spacecraft

Also Published As

Publication number Publication date
FR2373823B1 (en) 1980-09-05

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