Optimal Dynamic Inversion Control for Spacecraft Maneuver-Aided Tracking

@inproceedings{Jing2018OptimalDI,
  title={Optimal Dynamic Inversion Control for Spacecraft Maneuver-Aided Tracking},
  author={Zhongliang Jing and Han Pan and Yuankai Li and Peng Yu Dong},
  year={2018}
}
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… CONTINUE READING

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