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2018 | OriginalPaper | Chapter

17. Optimal Dynamic Inversion Control for Spacecraft Maneuver-Aided Tracking

Authors : Zhongliang Jing, Han Pan, Yuankai Li, Peng Dong

Published in: Non-Cooperative Target Tracking, Fusion and Control

Publisher: Springer International Publishing

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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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previous chapter Dynamic Optimal Sliding-Mode Control for Active Satellite Tracking
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Metadata
Title
Optimal Dynamic Inversion Control for Spacecraft Maneuver-Aided Tracking
Authors
Zhongliang Jing
Han Pan
Yuankai Li
Peng Dong
Copyright Year
2018
Book
Non-Cooperative Target Tracking, Fusion and Control

Print ISBN: 978-3-319-90715-4

Electronic ISBN: 978-3-319-90716-1

Copyright Year: 2018

DOI
https://doi.org/10.1007/978-3-319-90716-1_17

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