\({\mathcal{L}_1}\) Adaptive Loss Fault Tolerance Control of Unmanned Hypersonic Aircraft with Elasticity
نویسندگان
چکیده
This paper investigates the fault tolerance control of hypersonic aircrafts with L1 adaptive method in presence loss actuator effectiveness fault. The model considers uncertainties caused by features nonlinearities and couplings. Elasticity is taken into account vehicle modeling which makes more accurate. A velocity controller an altitude are designed to flexible PID as well for comparison. Finally, simulation results used analyze controller. Compared controller, controllers have better performance.
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ژورنال
عنوان ژورنال: Aerospace
سال: 2021
ISSN: ['2226-4310']
DOI: https://doi.org/10.3390/aerospace8070176