Finite-time Adaptive Attitude Tracking Fault-tolerant Control for Spacecraft
A finite-time adaptive attitude tracking fault-tolerant control method is proposed for non-rigid spacecraft with actuator fault, time-varying inertia and external disturbances. Firstly, based on the finite-time theory and adaptive approach, for overcoming the inertia uncertainties and rejecting the...
| Main Authors: | , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2019-02-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018043?st=article_issue |