1. Multiple Spacecraft Systems Coupled Attitude and Orbit Distributed Coordinated Tracking Control with Input Saturation.
- Author
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ZHANG Hai-bo, HU Qing-lei, MA Guang-fu, and ZHU Zhi-bin
- Subjects
- *
SPACE vehicles , *HYPERBOLIC processes , *CHEBYSHEV systems , *ARTIFICIAL neural networks , *TANGENT function - Abstract
Based on the consensus theory, distributed coordinated control for coupled relative orbits and attitudes of a multiple spacecraft system is investigated. With adoption of hyperbolic tangent function, more specifically, a distributed adaptive coordinated control algorithm is proposed for the case that the leader spacecraft state may only be available to only a subset of follower spacecrafts in the presence of input saturation constraints and external disturbances. Firstly, for the case that the leader spacecraft has the time-varying trajectory, three sliding-mode estimators are presented for each follower to obtain the estimates of the leader spacecraft's information. Then, for the case that the relative velocities and relative angular velocities among the follower spacecrafts are not measured, an adaptive law based on Chebyshev neural networks is proposed only using the leader's information. Furthermore, the distributed adaptive coordinated control algorithm with input saturation enables a fleet of followers to track the dynamic leader spacecraft. Simulation results illustrate effectiveness and feasibility of the proposed algorithm. [ABSTRACT FROM AUTHOR]
- Published
- 2013
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