JPH0375400B2 - - Google Patents

Info

Publication number
JPH0375400B2
JPH0375400B2 JP54099392A JP9939279A JPH0375400B2 JP H0375400 B2 JPH0375400 B2 JP H0375400B2 JP 54099392 A JP54099392 A JP 54099392A JP 9939279 A JP9939279 A JP 9939279A JP H0375400 B2 JPH0375400 B2 JP H0375400B2
Authority
JP
Japan
Prior art keywords
axis
spacecraft
momentum
angular momentum
rotor
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
JP54099392A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5539887A (en
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 filed Critical
Publication of JPS5539887A publication Critical patent/JPS5539887A/ja
Publication of JPH0375400B2 publication Critical patent/JPH0375400B2/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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect

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)
JP9939279A 1978-08-04 1979-08-02 Method of controlling direction of momentum stabilizing vehicle and direction control system Granted JPS5539887A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/931,172 US4275861A (en) 1978-08-04 1978-08-04 Orientation of momentum stabilized vehicles

Publications (2)

Publication Number Publication Date
JPS5539887A JPS5539887A (en) 1980-03-21
JPH0375400B2 true JPH0375400B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1991-11-29

Family

ID=25460325

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9939279A Granted JPS5539887A (en) 1978-08-04 1979-08-02 Method of controlling direction of momentum stabilizing vehicle and direction control system

Country Status (4)

Country Link
US (1) US4275861A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5539887A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA1114209A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2931612C3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4688746A (en) * 1984-11-05 1987-08-25 Cooper James W Satellite despin device
AT384592B (de) * 1985-12-31 1987-12-10 Morawetz Karl Einrichtung zum steuern von flugkoerpern
US4767084A (en) * 1986-09-18 1988-08-30 Ford Aerospace & Communications Corporation Autonomous stationkeeping for three-axis stabilized spacecraft
US4911385A (en) * 1987-04-30 1990-03-27 Agrawal Brij N Attitude pointing error correction system and method for geosynchronous satellites
US4824052A (en) * 1987-06-18 1989-04-25 Hughes Aircraft Company Nutation sensor and nutation control system for a dual-spin stabilized satellite
DE3729389A1 (de) * 1987-09-03 1989-03-16 Messerschmitt Boelkow Blohm Reakquisitionsverfahren fuer die nicklage eines erdsatelliten
US5012992A (en) * 1988-12-09 1991-05-07 Hughes Aircraft Company Spin stabilization via momentum wheels or similar devices
US5067084A (en) * 1989-05-25 1991-11-19 Honeywell Inc. Inertial measurement unit with aiding from roll isolated gyro
US5067673A (en) * 1990-02-07 1991-11-26 Hughes Aircraft Company Essentially passive method for inverting the orientation of a dual spin spacecraft
US5172876A (en) * 1990-08-03 1992-12-22 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
US5194872A (en) * 1990-11-14 1993-03-16 Charles Stark Draper Laboratory, Inc. Inertial navigation system with automatic redundancy and dynamic compensation of gyroscope drift error
US5667171A (en) 1995-04-28 1997-09-16 Hughes Aircraft Company Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device
US5826828A (en) * 1996-02-05 1998-10-27 Hughes Electronics Corporation Sun/earth acquisition without thrusters
US5921505A (en) * 1996-12-02 1999-07-13 Trw Inc. System and method for reducing mechanical disturbances from energy storage flywheels
US6032903A (en) * 1998-02-12 2000-03-07 Hughes Electronics Corporation Cooperative control structures and methods for satellite spin axis control
US6003818A (en) * 1998-03-11 1999-12-21 Hughes Electronics Corporation System and method for utilizing stored momentum to optimize spacecraft slews
FR2907423B1 (fr) * 2006-10-23 2009-07-03 Astrium Sas Soc Par Actions Si Gyrodyne et son dispositif de montage
US8571730B1 (en) * 2012-12-21 2013-10-29 Fukashi Andoh Attitude control device for in-space propellant depot
US8676407B1 (en) * 2013-01-22 2014-03-18 The Aerospace Corporation Energy-angular momentum diagnostic method for launch vehicle performance
US8571727B1 (en) * 2013-02-06 2013-10-29 The Aerospace Corporation Energy-angular momentum closed-loop guidance for launch vehicles

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3591108A (en) * 1967-01-27 1971-07-06 Rca Corp Control system for spinning bodies
US3940096A (en) * 1974-11-27 1976-02-24 Rca Corporation Re-orientation of a spacecraft relative to its angular momentum vector
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
JPS541600A (en) * 1977-06-07 1979-01-08 Mitsubishi Electric Corp System of varying attitude of artificial satellite

Also Published As

Publication number Publication date
US4275861A (en) 1981-06-30
JPS5539887A (en) 1980-03-21
DE2931612B2 (de) 1981-03-12
DE2931612A1 (de) 1980-02-21
CA1114209A (en) 1981-12-15
DE2931612C3 (de) 1981-11-05

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