Paper treats terminal guidance phase of 4-phase maneuver, object of which is to transfer commuter vehicle from its orbit to satellite orbit to meet satellite in soft contact fashion; relative motion between these two bodies is discussed, and steering equations are given; resulting trajectories are illustrated for various initial conditions.
Long-time satellite rendezvous trajectory
Aero/Space Eng
Aerospace Engineering ; 19 , n 6
1960
6 pages
Aufsatz (Zeitschrift)
Englisch
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