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Trajectory Optimization Applied to Space Rendezvous
Abstract:
The trajcetory plan problem of spece reandezvous mission was studied in this paper using nolinear optimization method. The optimization model was built based on the Hills equations. And by analysis property of the design variables, a transform was put forward , which eliminated the equation and nonlinear constraints as well as decreaseing the problem dimensions. The optimization problem was solved using Adaptive Simulated Annealing (ASA) method, and the rendezvous trajectory was designed.The method was validated by simulation results.
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3466-3470
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Online since:
September 2013
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© 2013 Trans Tech Publications Ltd. All Rights Reserved
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