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JPH0219040B2 - - Google Patents

Info

Publication number
JPH0219040B2
JPH0219040B2 JP51087715A JP8771576A JPH0219040B2 JP H0219040 B2 JPH0219040 B2 JP H0219040B2 JP 51087715 A JP51087715 A JP 51087715A JP 8771576 A JP8771576 A JP 8771576A JP H0219040 B2 JPH0219040 B2 JP H0219040B2
Authority
JP
Japan
Prior art keywords
roll
axis
yaw
satellite
error
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 - Lifetime
Application number
JP51087715A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5213300A (en
Inventor
Muuru Fueruda Ruudobitsuhi
Edoin Shumitsuto Junia Jooji
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 JPS5213300A publication Critical patent/JPS5213300A/ja
Publication of JPH0219040B2 publication Critical patent/JPH0219040B2/ja
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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP51087715A 1975-07-21 1976-07-21 Closed loop magnetic torque apparatus for roll and yaw error control of momentum biased satellite at low inclined locus Granted JPS5213300A (en)

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
JPS5213300A JPS5213300A (en) 1977-02-01
JPH0219040B2 true JPH0219040B2 (zh) 1990-04-27

Family

ID=26260420

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51087715A Granted JPS5213300A (en) 1975-07-21 1976-07-21 Closed loop magnetic torque apparatus for roll and yaw error control of momentum biased satellite at low inclined locus

Country Status (4)

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

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4424948A (en) * 1981-01-22 1984-01-10 Rca Corporation Magnetically torqued nutation damping
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 (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS498000A (zh) * 1972-03-27 1974-01-24
JPS50107700A (zh) * 1974-02-04 1975-08-25

Family Cites Families (5)

* 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
FR1602955A (zh) * 1968-06-25 1971-03-01
FR2023313B1 (zh) * 1968-10-01 1974-02-22 Hawker Siddeley Dynamics Ltd
JPS537720B1 (zh) * 1970-07-29 1978-03-20

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS498000A (zh) * 1972-03-27 1974-01-24
JPS50107700A (zh) * 1974-02-04 1975-08-25

Also Published As

Publication number Publication date
CA1073988A (en) 1980-03-18
DE2632864A1 (de) 1977-02-24
JPS5213300A (en) 1977-02-01
DE2632864C2 (de) 1982-08-12
FR2319150B1 (zh) 1982-11-12
FR2319150A1 (fr) 1977-02-18

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