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| Multi-objective optimization for spacecraft keeping on libration Halo orbit |
| Received:February 19, 2014 Revised:June 20, 2014 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7511/jslx201405001 |
| KeyWord:libration Halo orbit-keeping time-varying controller multiobjective optimization SiPESC software |
| Author | Institution |
| 杨春峰 |
大连理工大学 工业装备结构分析国家重点实验室 工程力学系, 大连 |
| 彭海军 |
大连理工大学 工业装备结构分析国家重点实验室 工程力学系, 大连 |
| 钟万勰 |
大连理工大学 工业装备结构分析国家重点实验室 工程力学系, 大连 |
| 陈飙松 |
大连理工大学 工业装备结构分析国家重点实验室 工程力学系, 大连 |
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| Abstract: |
| As the stabilization missions of the spacecraft on libration point Halo orbits of Sun-Earth system,energy consumption and orbit maintaining precision are their contradict objectives.This paper proposed a multi-objective optimization method to design time-varying controller in the Halo orbit stabilization missions.Firstly,a time-varying controller,based on the linearization CRTBP model,is constructed.Then,the weighting matrix elements of the controller are optimized with multi-objective algorithm.Finally,a study case,considering environment errors,is optimized and the Pareto fronts of the optimization results,showing the trade-off between the fuel consumption and orbit maintaining,prove the feasibility of this method. |
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