Relations are presented for space vehicle attitude control systems employing single-axis gyros; systems are compared with those using reactor wheels.
Basic response relations for attitude control using gyros
Joint Automatic Control Conference
Joint Automatic Control Conference ; 1963 Control
Joint Automatic Control Conference ; p 645-646
1963
2 pages
Aufsatz (Konferenz)
Englisch
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Basic response relations for satellite attitude control using gyros
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