This paper studies the distributed adaptive control of a team of underactuated flexible spacecraft under a leader–follower architecture with the measurements of the rigid bodies only. By treating the flexible spacecraft as an underactuated Lagrange system, an adaptive control strategy is proposed with the feedback of the generalized coordinates, velocities, and accelerations of the rigid bodies. Then, an extended state observer is introduced to design a distributed adaptive controller without the measurement of the generalized accelerations.
Distributed Adaptive Attitude Control for Networked Underactuated Flexible Spacecraft
IEEE Transactions on Aerospace and Electronic Systems ; 55 , 1 ; 215-225
2019-02-01
2379430 byte
Article (Journal)
Electronic Resource
English
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