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A novel nonlinear resilient control for a quadrotor UAV via backstepping control and nonlinear disturbance observer

机译:基于反步控制和非线性扰动观测器的四旋翼无人机新型非线性弹性控制

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摘要

This study proposes a novel nonlinear resilient trajectory control for a quadrotor unmanned aerial vehicle (UAV) using backstepping control and nonlinear disturbance observer. First, a nonlinear dynamic model for the quadrotor UAV that considers external disturbances from wind model uncertainties is developed. A nonlinear disturbance observer is then constructed separately from the controller to estimate the external disturbances and compensate for the negative effects of the disturbances. Based on the estimates from the given observer, a nominal nonlinear backstepping trajectory-tracking position controller is designed to stabilize the subsystems step by step until the ultimate control law is obtained. An extra term is added to the nominal controller to address the problem of actuator effectiveness loss and to ensure system resilience. The stability of the resilient controller is analyzed using Lyapunov stability theory. Simulation results are presented to demonstrate the effectiveness and robustness of the proposed nonlinear resilient controller.
机译:这项研究提出了一种新颖的非线性弹性轨迹控制的四旋翼无人机(UAV)使用反推控制和非线性干扰观测器。首先,开发了一种四旋翼无人机的非线性动力学模型,该模型考虑了来自风模型不确定性的外部干扰。然后,与控制器分开构造非线性干扰观测器,以估计外部干扰并补偿干扰的负面影响。基于给定观察者的估计,设计了名义上的非线性反步轨迹跟踪位置控制器,以逐步稳定子系统,直到获得最终控制律。在标称控制器上增加了一个额外的术语,以解决执行器效率损失的问题并确保系统的弹性。使用Lyapunov稳定性理论分析了弹性控制器的稳定性。仿真结果表明了所提出的非线性弹性控制器的有效性和鲁棒性。

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