L1 Adaptive for Aircraft Lateral Fault Tolerant Control with Actuator Failure
When aircraft is laterally controlled, actuator failure may cause matched/unmatched uncertainties. In order to deal with the uncertainty, a fault-tolerant controller is designed by using L1 adaptive control method. An aircraft lateral model was established by considering faults and disturbances, the...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2019-10-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2019/05/jnwpu2019375p935/jnwpu2019375p935.html |