Multiple impulsive spacecraft formation reconfiguration based on the orbital element differences dynamics model

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	Multiple impulsive spacecraft formation reconfiguration based on the orbital element differences dynamics model
	Youliang, Wang 1; Mingtao, Li 1,2; Yazhe, Meng 3; Jianhua, Zheng 1,2
作者部门	空间技术部
会议录名称	Advances in the Astronautical Sciences
	2018
卷号	165
页码	53-66
语种	英语
ISSN号	0065-3438
ISBN号	9780877036531
摘要	Multiple impulsive spacecraft formation reconfiguration under J2 perturbation is studied, and the fuel-optimal strategy is developed based on nonsingular Gauss Variation Equation and mean orbital element propagation under J2 perturbation. Firstly, a linear relative dynamics equation using the nonsingular orbital element differences dynamics model is derived, which considers the J2 perturbation and the coupling effects between in-plane and out-of-plane relative motion. Thus, the formation reconfiguration problem can be described as a Mixed Integer Nonlinear Programming mathematical problem. Then, the hybrid approach of Differential Evolution algorithm and Sequence Quadratic Programming is proposed to optimize the total velocity increment. Finally, the efficient of the optimization result is proved with the Primer Vector Theory considering J2 perturbation, and the influence of transfer time and the reference orbital eccentricity on the total velocity increment is analyzed. The simulation results show that the hybrid approach is effective, and can obtain the feasible solution efficiently for both circular and elliptic reference orbit. © 2018 KASHYAP.
会议名称	4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018
会议日期	May 21, 2018 - May 23, 2018
会议地点	Changsha, China
收录类别	EI
文献类型	会议论文
条目标识符	http://ir.nssc.ac.cn/handle/122/6683
专题	空间技术部
通讯作者	Youliang, Wang
作者单位	1.University of Chinese Academy of Sciences, Beijing; 100049, China; 2.National Space Science Center, Chinese Academy of Sciences, Beijing; 100190, China; 3.School of Aerospace Engineering, Tsinghua University, Beijing; 100084, China
推荐引用方式 GB/T 7714	Youliang, Wang,Mingtao, Li,Yazhe, Meng,et al. Multiple impulsive spacecraft formation reconfiguration based on the orbital element differences dynamics model[C],2018:53-66.