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- Title
L 1 Adaptive Loss Fault Tolerance Control of Unmanned Hypersonic Aircraft with Elasticity.
- Authors
Li, Zhaoying; Shi, Shuai
- Abstract
This paper investigates the fault tolerance control of hypersonic aircrafts with L 1 adaptive control method in the presence of loss of actuator effectiveness fault. The hypersonic model considers the uncertainties caused by the features of nonlinearities and couplings. Elasticity is taken into account in hypersonic vehicle modeling which makes the model more accurate. A velocity L 1 adaptive controller and an altitude L 1 adaptive controller are designed to control flexible hypersonic vehicle model with actuator loss fault. A PID controller is designed as well for comparison. Finally, the simulation results are used to analyze the effectiveness of the controller. Compared to the results of PID controller, L 1 controllers have better performance.
- Subjects
HYPERSONIC planes; ADAPTIVE control systems; PID controllers; ELASTICITY; VEHICLE models; ALTITUDES; FAULT-tolerant control systems; FAULT-tolerant computing
- Publication
Aerospace (MDPI Publishing), 2021, Vol 8, Issue 7, p176
- ISSN
2226-4310
- Publication type
Article
- DOI
10.3390/aerospace8070176