Adaptive Backstepping Attitude Control Law with L2-Gain Performance for Flexible Spacecraft

In this paper, an observer-based adaptive backstepping attitude maneuver controller (briefly, OBABC) for flexible spacecraft is presented. First, an observer is constructed to estimate the flexible modal variables. Based on the proposed observer, a backstepping control law is presented for the case...

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Bibliographic Details
Main Authors: Rui-Qi Dong, Yu-Yao Wu, Ying Zhang, Ai-Guo Wu
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/6392175
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