Application of Hamiltonian structure-preserving control to formation flying on a J 2-perturbed mean circular orbit

2012 ◽  
Vol 113 (4) ◽  
pp. 403-433 ◽  
Author(s):  
Ming Xu ◽  
Jiamin Zhu ◽  
Tian Tan ◽  
Shijie Xu
Keyword(s):  
Circular Orbit ◽  
Hamiltonian Structure ◽  
Formation Flying ◽  
Structure Preserving

Capturing a spacecraft around a flyby asteroid using Hamiltonian-structure-preserving control

2021 ◽  
Vol 93 ◽  
pp. 105500
Author(s):  
Ming Xu ◽  
Qingyu Qu ◽  
Yunfeng Dong ◽  
Yaru Zheng ◽  
Ramil Santos
Keyword(s):  
Hamiltonian Structure ◽  
Structure Preserving

A Model Predictive Controller of Spacecraft Formation Tracking Based on the Hill Equation

2013 ◽  
Vol 380-384 ◽  
pp. 270-273
Author(s):  
Yan Kai Wang ◽  
Chong Zhang ◽  
Ying Hong Zhao
Keyword(s):  
Circular Orbit ◽  
Formation Flying ◽  
Control Method ◽  
Hill Equation ◽  
Spacecraft Formation ◽  
Spacecraft Formation Flying ◽  
Formation Tracking ◽  
Predictive Controller ◽  
Orbit Tracking ◽  
The Hill

Spacecraft formation flying has higher performance, higher reliability and lower costs comparing to the traditional single spacecraft. So it becomes a research hotspot in the field of aerospace in China and abroad over the past decade. This paper focuses on the orbital maintenance control between the following spacecraft and the main spacecraft. On the basis of circular orbit or nearly circular orbit, this paper studied the relative motion of spacecraft formation flying based on the Hill equation without considering the influence of the perturbation factor, when the distance between spacecrafts is close. This paper used the generalized predictive control method to design a controller of spacecraft formation tracking. By using Matlab/Simulink, the simulation results showed that the spacecraft has a good orbit tracking capability and a strong anti-interference ability.

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