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Proceedings Paper

Application of particle swarm optimization technique in optimal parameters determination of the spacecraft remote rendezvous
Author(s): Qiyu Wang; Jianping Yuan; Zhanxia Zhu
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Paper Abstract

Beginning with the mathematics model of the spacecrafts remote rendezvous, we research the problem of space maneuver vehicle (SMV) remote rendezvous on-orbit target basing on Lambert orbit maneuver method. To find a minimum velocity impulse transfer orbit, we set up object functions when the SMV's initial orbit parameters are known or unknown. We use an advanced intelligent optimal technology, particle swarm optimal technology, to get the object function's extremum. So we can obtain the SMV's proper initial orbit parameters and transfer occasion. On this condition the SMV needs little velocity impulse to approach the target spacecraft. Last, the simulation results show that we can get a transfer orbit to rapidly approaching on-orbit target which needs very little velocity impulse by using this method.

Paper Details

Date Published: 14 November 2007
PDF: 7 pages
Proc. SPIE 6789, MIPPR 2007: Medical Imaging, Parallel Processing of Images, and Optimization Techniques, 67892A (14 November 2007); doi: 10.1117/12.749844
Show Author Affiliations
Qiyu Wang, Northwestern Polytechnical Univ. (China)
Jianping Yuan, Northwestern Polytechnical Univ. (China)
Zhanxia Zhu, Northwestern Polytechnical Univ. (China)

Published in SPIE Proceedings Vol. 6789:
MIPPR 2007: Medical Imaging, Parallel Processing of Images, and Optimization Techniques
Jianguo Liu; Kunio Doi; Patrick S. P. Wang; Qiang Li, Editor(s)

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