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OPTIMAL RENDEZVOUS BETWEEN TWO SPACECRAFTS USING TWO IMPULSES
Author(s): 
Pages: 14-23
Year: Issue:  2
Journal: Aerospace Control

Keyword:  Spacecraft~+Optimal rendezvous;
Abstract: The eptimal analytic solution that minimizes the sum of the applied impulses necessary to ren- dezvous is obtained for the Clohessy-Wiltshire equations presented by authors in the reference[1] with a linear gravity model assumption.Numerical computations are conducted to verify the optimal solution algorithm.
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