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Proceedings Paper

The guidance method of differential game for orbiter under target maneuvering based on orbital elements
Author(s): Qiu-hua Zhang; Yi Sun; Ming-ming Huang
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Paper Abstract

The rendezvous problem was analyzed by the guidance method of qualitative differential game for space vehicle while the target is maneuvering, based upon the perturbation equation of orbital elements. By taking into account of fuel assumption for rendezvous control process under radial thrust, we introduced the performance index for quantitative differential game into Hamiltonian function to resolve the guidance problems for maneuvering space vehicle for orbit approaching, and gave a set of theoretical solution, barriers and an example for simulation. From mathematically simulation it is verified that there are the barriers in the method for the target maneuvering.

Paper Details

Date Published: 31 May 2006
PDF: 12 pages
Proc. SPIE 6221, Modeling, Simulation, and Verification of Space-based Systems III, 62210F (31 May 2006); doi: 10.1117/12.664854
Show Author Affiliations
Qiu-hua Zhang, Harbin Institute of Technology (China)
Yi Sun, Harbin Institute of Technology (China)
Ming-ming Huang, Harbin Institute of Technology (China)


Published in SPIE Proceedings Vol. 6221:
Modeling, Simulation, and Verification of Space-based Systems III
Pejmun Motaghedi, Editor(s)

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