Performance and optimization of satellite borne terminal acquisition and associated external gross guidance systems for effecting rendezvous of orbiting space stations are investigated; broadly applicable analysis of influence of relative trajectories and error in information output of vectoring and control environment is developed; special case of general search theorem is demonstrated.
Controlled rendezvous of orbiting space stations
ARS J
ARS Journal ; 31 , n 8
1961
7 pages
Aufsatz (Zeitschrift)
Englisch
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