USB511346I5 - - Google Patents

Info

Publication number
USB511346I5
USB511346I5 US51134674A USB511346I5 US B511346 I5 USB511346 I5 US B511346I5 US 51134674 A US51134674 A US 51134674A US B511346 I5 USB511346 I5 US B511346I5
Authority
US
United States
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.)
Pending
Application number
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
Priority to US05/511,346 priority Critical patent/US3984072A/en
Publication of USB511346I5 publication Critical patent/USB511346I5/en
Application granted granted Critical
Publication of US3984072A publication Critical patent/US3984072A/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • 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
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors

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)
US05/511,346 1974-10-02 1974-10-02 Attitude control system Expired - Lifetime US3984072A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/511,346 US3984072A (en) 1974-10-02 1974-10-02 Attitude control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/511,346 US3984072A (en) 1974-10-02 1974-10-02 Attitude control system

Publications (2)

Publication Number Publication Date
USB511346I5 true USB511346I5 (en) 1976-01-27
US3984072A US3984072A (en) 1976-10-05

Family

ID=24034501

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/511,346 Expired - Lifetime US3984072A (en) 1974-10-02 1974-10-02 Attitude control system

Country Status (1)

Country Link
US (1) US3984072A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111046499A (en) * 2019-12-27 2020-04-21 北京中科宇航探索技术有限公司 A method and system for determining the installation position of a rate gyroscope

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4085440A (en) * 1977-05-05 1978-04-18 The United States Of America As Represented By The Secretary Of The Army Inertial navigation system
FR2403925A2 (en) * 1977-09-23 1979-04-20 Alphen Jacques DEVICE FOR AUTOMATIC CORRECTION OF THE ORIENTATION OF THE LIGHT BEAM OF A MOTORCYCLE OR SIMILAR VEHICLE HEADLIGHT
FR2486675A1 (en) * 1980-07-09 1982-01-15 Aerospatiale METHOD AND SYSTEM FOR SERVING A MOBILE PLATFORM MOUNTED ON BOARD A SPATIAL VEHICLE
US4437047A (en) 1981-07-13 1984-03-13 Hughes Aircraft Company System for autonomous earth-pointing acquisition of a dual-spin satellite
US6254030B1 (en) * 1983-11-17 2001-07-03 Lockheed Martin Corporation Vehicle guidance system for guided missiles having adaptive trajectory bias
US4659035A (en) * 1985-01-25 1987-04-21 The United States As Represented By The Secretary Of The Navy Rate estimation by mixing two independent rate signals
US4765573A (en) * 1987-04-29 1988-08-23 Raytheon Company Method of compensation for friction in a stabilized platform
US5050087A (en) * 1989-11-29 1991-09-17 Westinghouse Electric Corp. System and method for providing accurate attitude measurements at remote locations within an aircraft
FR2666561B1 (en) * 1990-09-06 1995-06-09 Aerospatiale PROCESS FOR DRIVING A SPACE MACHINE WITH A PRECESSION MOVEMENT AND DEVICE FOR IMPLEMENTING SAME.
US6102337A (en) * 1995-12-22 2000-08-15 Hughes Electronics Corporation Spacecraft attitude control with gimbaled thrusters
US5886257A (en) * 1996-07-03 1999-03-23 The Charles Stark Draper Laboratory, Inc. Autonomous local vertical determination apparatus and methods for a ballistic body
US6308911B1 (en) * 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6373023B1 (en) 1999-03-02 2002-04-16 General Dynamics (Ots) Aerospace, Inc. ARC discharge initiation for a pulsed plasma thruster
US7185857B2 (en) * 2004-01-28 2007-03-06 Honeywell International, Inc. Thrust vector actuation control system and method
US7590481B2 (en) * 2005-09-19 2009-09-15 Ford Global Technologies, Llc Integrated vehicle control system using dynamically determined vehicle conditions
US8838336B2 (en) * 2010-07-29 2014-09-16 Hitachi Automotive Systems, Ltd. Vehicle body attitude control apparatus

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3301508A (en) * 1961-06-07 1967-01-31 United Aircraft Corp Guidance system with stellar correction
NL267419A (en) * 1961-07-07
US3132828A (en) * 1962-12-26 1964-05-12 Honeywell Regulator Co Dirigible craft control apparatus and method
GB1157685A (en) * 1965-07-31 1969-07-09 Contraves Italiana Spa Piloting apparatus for a Missile Adapted to Damp Pitching of the Missile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111046499A (en) * 2019-12-27 2020-04-21 北京中科宇航探索技术有限公司 A method and system for determining the installation position of a rate gyroscope
CN111046499B (en) * 2019-12-27 2023-08-04 广州中科宇航探索技术有限公司 Method and system for determining installation position of rate gyro

Also Published As

Publication number Publication date
US3984072A (en) 1976-10-05

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