MATEC Web Conf.
Volume 114, 20172017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017)
|Number of page(s)||10|
|Section||Chapter 4: Interdisciplinary|
|Published online||10 July 2017|
Revisiting the two-side optimization problem in satellite pursuit-evasion
1 ShangHai Institute of Microsystem and Information Technology, ShangHai 200050, China
2 University of Chinese Academy of Sciences, BeiJing 100049, China
3 ShangHai Engineering Center for Microsatellite, ShangHai 201210, China
4 Harbin Institute of Technology, Harbin 150001, China
a Corresponding author: firstname.lastname@example.org
In the present paper two-side optimization problem where the intercepting satellite pursuits the target satellite was studied. In the pursuit-evasion game the continuous thruster and the simple central gravity with J2 perturbation were involved for two satellites. With applying the functional extremum condition, the optimal control outputs of both side satellites were obtained by building the systems Hamilton function. Further, the two side optimal problem was transformed to the TPBVP, which contributed the solution with the mixed numerical method. Finally, the proposed method was validated by the numerical simulation, where the optimal interception and escaping trajectories were illustrated.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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