BE739696A - - Google Patents

Info

Publication number
BE739696A
BE739696A BE739696DA BE739696A BE 739696 A BE739696 A BE 739696A BE 739696D A BE739696D A BE 739696DA BE 739696 A BE739696 A BE 739696A
Authority
BE
Belgium
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
Priority claimed from GB5875968A external-priority patent/GB1279098A/en
Application filed filed Critical
Publication of BE739696A publication Critical patent/BE739696A/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/32Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/166Mechanical, construction or arrangement details of inertial navigation systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
BE739696D 1968-10-01 1969-10-01 BE739696A (da)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB5875968A GB1279098A (en) 1968-10-01 1968-10-01 Improvements in orbiting spacecraft or satellite attitude control systems
GB4660868 1968-10-01

Publications (1)

Publication Number Publication Date
BE739696A true BE739696A (da) 1970-03-16

Family

ID=26265857

Family Applications (1)

Application Number Title Priority Date Filing Date
BE739696D BE739696A (da) 1968-10-01 1969-10-01

Country Status (4)

Country Link
BE (1) BE739696A (da)
DE (1) DE1950332A1 (da)
FR (1) FR2023313B1 (da)
NL (1) NL6914824A (da)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3834653A (en) * 1972-03-27 1974-09-10 Rca Corp Closed loop roll and yaw control for satellites
US3937423A (en) * 1974-01-25 1976-02-10 Hughes Aircraft Company Nutation and roll error angle correction means
CA1073988A (en) * 1975-07-21 1980-03-18 Ludwig Muhlfelder Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits

Also Published As

Publication number Publication date
DE1950332A1 (de) 1970-06-11
NL6914824A (da) 1970-04-03
FR2023313A1 (da) 1970-08-21
FR2023313B1 (da) 1974-02-22

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