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