Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8056443 | Acta Astronautica | 2015 | 11 Pages |
Abstract
The controllers are derived using the Lyapunov theory, so the stability of the closed-loop system is guaranteed. Moreover, the modified controllers are provided to alleviate the chattering phenomenon and eliminate the singular problem. Finally, simulation results are given to demonstrate the efficiency of the proposed methods.
Keywords
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Jiwei Gao, Yuanli Cai,