Small strapdown inertial system employing dry tuned rotary suspension gyroscopes for application to aircraft and ship navigation, high-accuracy space attitude reference and booster guidance. Two gyros provide for 3 axis sensing, leaving the 4th axis available from the pair of 2 axis instruments redundant.
Strapdown guidance system developed
Aviation Week and Space Technology ; 96 , 12 ; 59
1972
1 Seite
Article (Journal)
English
Strapdown guidance component research
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