Attitude Control Of A Spacecraft With A Strapdown Inertial Reference System And Onboard Computer
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A strapdown inertial reference system and an onboard digital computer can be used to change the attitude of a spacecraft over large angles in an arbitrary direc
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Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has
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Pages: 1064
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Type: BOOK - Published: 1970 - Publisher: