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Optimal Control Law Design for Safe Rendezvous and Docking of Between Two Spacecrafts
Author(s): 
Pages: 13-19
Year: Issue:  3
Journal: Aerospace Control

Keyword:  RendezvousDockingOptimal control;
Abstract: Safe control problems during the final phase of rendezvous and docking between twospacecrafts are studied Controls are assumed to be constant. A near time--optimal feedbackcontrol law is presented by using decentralized optimal control scheme. Simulation results areshown to illustrate effectiveness of the control law.
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