Optimal Multiple-Impulse Noncoplanar Rendezvous Trajectory Planning Considering the J2 Perturbation Effects

Author:

Xu Guangde,He Zongbo,Zhao Huiguang,Zhang Qiang,Xing Yanjun,Feng Cong

Publisher

Springer Nature Singapore

Reference8 articles.

1. Hughes, S.P., Mailhe, L.M., Guzman, J.J.: A comparison of trajectory optimization methods for the impulsive minimum fuel rendezvous problem. Advances in the Astronautical Sciences, 113 (2003)

2. Abdelkhalik, O., Mortari, D.: N-impulse orbit transfer using genetic algorithms. J. Spacecraft and Rockets, 44(2), 456–460 (2007)

3. Chen, Q., Yang, Z., Luo, Y.: Optimization of multi-impulse orbit transfer based on particle swarm optimization algorithm. Aerospace Control Appl. 40(5), 25–30 (2014)

4. Liu, Y., Xiao, Y.E., Hao, Y., et al.: Optimization of transfer orbit for multiple-pulse noncoplanar rendezvous and docking. Optics and Precision Eng. 25, 987-998 (2017)

5. Zhou, J., Chang, Y.: Optimal multiple-impulse rendezvous between non-coplanar elliptic orbits considering the J2 perturbation effects. Journal of Astronautics 29(2), 472-475 (2008)

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