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Multiple impulsive spacecraft formation reconfiguration based on the orbital element differences dynamics model
Youliang, Wang1; Mingtao, Li1,2; Yazhe, Meng3; Jianhua, Zheng1,2
Department空间技术部
Source PublicationAdvances in the Astronautical Sciences
2018
Volume165
Pages53-66
Language英语
ISSN0065-3438
ISBN9780877036531
AbstractMultiple 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.
Conference Name4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018
Conference DateMay 21, 2018 - May 23, 2018
Conference PlaceChangsha, China
Indexed ByEI
Document Type会议论文
Identifierhttp://ir.nssc.ac.cn/handle/122/6683
Collection空间技术部
Corresponding AuthorYouliang, Wang
Affiliation1.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
Recommended Citation
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.
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