Robust fault diagnosis and fault-tolerant control for nonlinear quadrotor unmanned aerial vehicle system with unknown actuator faults
نویسندگان
چکیده
This article addresses the problem that quadrotor unmanned aerial vehicle (UAV) actuator faults, including small-amplitude bias faults and gain degradation, cannot be detected in time. A hybrid observer, which combines fast convergence from adaptive observer strong robustness sliding mode is proposed to detect estimate UAV accurately with model uncertainties disturbances. nonlinear disturbances considered a more precise unified expression for do not require knowing where upper or lower bound provided. The original system decomposed into two subsystems by coordinate transformation improve detection accuracy small amplitude avoid external influences. then designed subsystem states good stability selecting Lyapunov function. fault-tolerant controller obtained depending on fault estimation compensating normal (proportion integral differential [PID] controller). Several numerical simulations confirmed unknown can detected, estimated, compensated even under disturbance conditions.
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ژورنال
عنوان ژورنال: International Journal of Advanced Robotic Systems
سال: 2021
ISSN: ['1729-8806', '1729-8814']
DOI: https://doi.org/10.1177/17298814211002734