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Alternative TitleMultiple impulsive trajectory optimization of satellite formation reconfiguration under J2 perturbation
王有亮1,2,3; 郑建华1,2,3; 李明涛1,2,3
Source Publication国防科技大学学报
Keyword椭圆参考轨道 编队重构 多脉冲轨迹优化 J2摄动 高斯变分方程


Other Abstract

Arming at the formation reconfiguration problem for the elliptic reference orbit under J2 perturbation, a multiple impulsive trajectory optimization strategy was developed on the basis of the Gauss variation equation and with the objective function of minimal fuel consumption. A relative dynamics equation using the orbital element difference was derived, in which the J2 perturbation and the coupling effects between in-plane and out-of-plane relative movements were considered. The hybrid approach of the genetic algorithm and the sequence quadratic programming was proposed to optimize the total velocity increment. The simulation results show that the hybrid approach is effective, and can obtain the feasible solution efficiently. Since the J2 perturbation and elliptic reference orbit are considered in the study, the approach has some reference significance for the trajectory optimization of space mission. © 2018, NUDT Press. All right reserved.

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Document Type期刊论文
Affiliation1.中国科学院 国家空间科学中心,北京 100190;
2.中国科学院 复杂航天系统电子信息技术重点实验室, 北京 100190;
3.中国科学院大学, 北京 100049
Recommended Citation
GB/T 7714
王有亮,郑建华,李明涛. J2摄动下卫星编队重构的多脉冲轨迹优化[J]. 国防科技大学学报,2018,40(6):1-8.
APA 王有亮,郑建华,&李明涛.(2018).J2摄动下卫星编队重构的多脉冲轨迹优化.国防科技大学学报,40(6),1-8.
MLA 王有亮,et al."J2摄动下卫星编队重构的多脉冲轨迹优化".国防科技大学学报 40.6(2018):1-8.
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