Abstract：Based on Unscented filtering method and Huber robust filtering method, an adaptive robust relative navigation Huber-UKF filter is obtained. Besides, the second-order sliding model control in terms of the twist algorithm is used to design the relative orbital controller and the robustness of the system is increased. Simulation results demonstrate the relative navigation method and relative orbital control algorithm are applied to the precise formation flying with the target
on elliptical orbit and are robust to the thrust fault of the chase spacecraft.
冯刚, 杨东春, 颜根廷. 近程编队飞行鲁棒非线性导航滤波器设计及相对路径控制[J]. 指挥与控制学报, 2015, 1(2): 181-191.
FENG Gang, YANG Dong-Chun, YAN Gen-Ting. An Adaptive Robust Nonlinear Relative Navigation Filter and Relative Orbital Controller Applied to Formation Flying. Journal of Command and Control, 2015, 1(2): 181-191.
2015, Vol. 1 
