FR2319150A1 - Dispositif de stabilisation pour satellite en orbite synchrone - Google Patents

Dispositif de stabilisation pour satellite en orbite synchrone

Info

Publication number
FR2319150A1
FR2319150A1 FR7621997A FR7621997A FR2319150A1 FR 2319150 A1 FR2319150 A1 FR 2319150A1 FR 7621997 A FR7621997 A FR 7621997A FR 7621997 A FR7621997 A FR 7621997A FR 2319150 A1 FR2319150 A1 FR 2319150A1
Authority
FR
France
Prior art keywords
roll
torque generator
yaw
phase detector
horizontal sensor
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
FR7621997A
Other languages
English (en)
Other versions
FR2319150B1 (fr
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.)
RCA Corp
Original Assignee
RCA Corp
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
Priority claimed from GB30390/75A external-priority patent/GB1544083A/en
Application filed by RCA Corp filed Critical RCA Corp
Publication of FR2319150A1 publication Critical patent/FR2319150A1/fr
Application granted granted Critical
Publication of FR2319150B1 publication Critical patent/FR2319150B1/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
    • B64G1/36—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
    • B64G1/244—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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR7621997A 1975-07-21 1976-07-19 Dispositif de stabilisation pour satellite en orbite synchrone Granted FR2319150A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB30390/75A GB1544083A (en) 1975-07-21 1975-07-21 Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits
US05/640,147 US4062509A (en) 1975-07-21 1975-12-12 Closed loop roll/yaw control system for satellites

Publications (2)

Publication Number Publication Date
FR2319150A1 true FR2319150A1 (fr) 1977-02-18
FR2319150B1 FR2319150B1 (fr) 1982-11-12

Family

ID=26260420

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7621997A Granted FR2319150A1 (fr) 1975-07-21 1976-07-19 Dispositif de stabilisation pour satellite en orbite synchrone

Country Status (4)

Country Link
JP (1) JPS5213300A (fr)
CA (1) CA1073988A (fr)
DE (1) DE2632864C2 (fr)
FR (1) FR2319150A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498155A1 (fr) * 1981-01-22 1982-07-23 Rca Corp Procede et appareil permettant d'amortir la nutation par application d'un couple magnetique dans la commande d'un engin spatial

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5851319A (ja) * 1981-09-24 1983-03-26 Ricoh Co Ltd 定電圧電源装置
DE3214373A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und einrichtung fuer die lageregelung eines satelliten

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2023313A1 (fr) * 1968-10-01 1970-08-21 Hawker Siddeley Dynamics Ltd
FR1602955A (fr) * 1968-06-25 1971-03-01
FR2103808A5 (fr) * 1970-07-29 1972-04-14 Tokyo Shibaura Electric Co

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3232561A (en) * 1963-06-06 1966-02-01 Honeywell Inc Control apparatus for space craft
US3429524A (en) * 1965-07-19 1969-02-25 Westinghouse Electric Corp Attitude control system
US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
JPS50107700A (fr) * 1974-02-04 1975-08-25

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1602955A (fr) * 1968-06-25 1971-03-01
FR2023313A1 (fr) * 1968-10-01 1970-08-21 Hawker Siddeley Dynamics Ltd
FR2103808A5 (fr) * 1970-07-29 1972-04-14 Tokyo Shibaura Electric Co

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498155A1 (fr) * 1981-01-22 1982-07-23 Rca Corp Procede et appareil permettant d'amortir la nutation par application d'un couple magnetique dans la commande d'un engin spatial

Also Published As

Publication number Publication date
JPH0219040B2 (fr) 1990-04-27
DE2632864A1 (de) 1977-02-24
FR2319150B1 (fr) 1982-11-12
JPS5213300A (en) 1977-02-01
DE2632864C2 (de) 1982-08-12
CA1073988A (fr) 1980-03-18

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