Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Low thrust station keeping guidance for a 24- hour satellite.
GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE ; 1968 ; PASADENA, CA
1968-08-01
Conference paper
No indication
English
NTRS | 1972
|NTIS | 1972
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