Non-initial Value Fault-Tolerant Prescribed Performance Control for Small Fixed-Wing UAVs with Actuator Faults

Bo Huang; Zhonghua Wu

doi:10.1007/978-981-96-2244-3_29

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Non-initial Value Fault-Tolerant Prescribed Performance Control for Small Fixed-Wing UAVs with Actuator Faults

Bo Huang Zhonghua Wu

Year: 2025 Lecture notes in electrical engineering Pages: 295-303 Publisher: Springer Science+Business Media

DOI: 10.1007/978-981-96-2244-3_29

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Keywords:

Fixed wing Control theory (sociology) Fault tolerance Actuator Wing Computer science Control (management) Engineering Structural engineering Distributed computing Artificial intelligence

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Adaptive Control of Nonlinear Systems

Physical Sciences → Engineering → Control and Systems Engineering

Fault Detection and Control Systems

Physical Sciences → Engineering → Control and Systems Engineering

Adaptive Dynamic Programming Control

Physical Sciences → Computer Science → Computational Theory and Mathematics

Non-initial Value Fault-Tolerant Prescribed Performance Control for Small Fixed-Wing UAVs with Actuator Faults

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