Systems analysis approach to problems involved in obtaining and maintaining 24-hr equatorial satellite; consideration of orbit ascent, initial longitude positioning, and control of satellite drift away from desired stationary longitude; orbit control system, including ground based tracking and command stations, computations and control center, and satellite subsystems, which will provide satisfactory stationary orbit is synthesized; capability of control system was tested by computer simulation; results indicate that synthesized system provides satisfactory stationary orbit in presence of likely system errors.
Longitude positioning and orbit control of 24-hour equatorial satellite
AIAA J
AIAA Journal ; 2 , n 6
1964
9 pages
Aufsatz (Zeitschrift)
Englisch
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AIAA | 2010
|Attitude control and station keeping of communication satellite in 24-hour orbit
Engineering Index Backfile | 1963
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