Abstract
The discussion of this chapter is focused on a generalized inter-satellite tracking problem, maneuver-aided active satellite tracking. Due to the uncooperative maneuver of the active target satellite decreasing the tracking performance, a generalized scheme named spacecraft maneuver-aided tracking strategy (SMATS) is established. The SMATS is mainly composed of an algorithm for robust tracking, a scheme for reference coordinate system matching, a relative motion control law, and a transfer function of tracking attitude. It can help realize the chaser satellite staying autonomously with the desired position and attitude and guarantee the tracking performance. The control law is developed by using the optimal dynamic inversion control (ODIC) method, having six DOFs. Based on the precise feedback linearization, the ODIC law is a nonlinear optimal solution, providing desirable control performance. The efficiency of the SMATS and the advantages of the ODIC law are demonstrated by several simulation cases.
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Acknowledgements
This work was supported in part by Natural Science Foundation of China (61175028, 60775022 and 60674107) and Aviation Science Foundation of China (2009ZC57003), and in part by the Canada Research Chair program.
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Jing, Z., Pan, H., Li, Y., Dong, P. (2018). Optimal Dynamic Inversion Control for Spacecraft Maneuver-Aided Tracking. In: Non-Cooperative Target Tracking, Fusion and Control. Information Fusion and Data Science. Springer, Cham. https://doi.org/10.1007/978-3-319-90716-1_17
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DOI: https://doi.org/10.1007/978-3-319-90716-1_17
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