Closed optimal solution of special rendezvous problem; problem is considered assuming that passive circular orbiting vehicle is uncontrolled, active spacecraft has main rocket engine and additional control nozzles, and that main rocket engine thrust, and direction be constant during maneuver; fuel bottleneck is control nozzles' consumption; optimization problem is solved in closed form; for some classes of initial conditions optimal solutions are given; evaluation of optimal solution requires only elementary calculations. (45567)
Die strenge optimale Loesung eines speziellen Rendezvous-problems
Die strenge optimale Loesung eines speziellen Rendezvous-problems
Zeitschrift fuer Flugwissenschaften ; 16 , n 4
1968
6 pages
Aufsatz (Zeitschrift)
Deutsch
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