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Robust adaptive backstepping control for unmanned autonomous helicopter with flapping dynamics

机译:具有拍打动力学的无人驾驶直升机的鲁棒自适应反推控制

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In this paper, a robust adaptive backstepping control scheme is studied for attitude and altitude control of medium-scale unmanned autonomous helicopter (UAH) with flapping dynamics. A simplified UAH model is established and nonlinear disturbance observer (NDO) is designed to eliminate the effect of unknown external disturbance. The robust adaptive backstep-ping approach is employed to design the attitude and altitude controller for the outputs tracking the desired trajectory. The stability of the closed-loop system is proved via Lyapunov analysis and all closed-loop signals are uniformly ultimately bounded. Simulation results are presented to demonstrate the effectiveness of the developed control method.
机译:本文研究了一种鲁棒的自适应反推控制方案,用于具有扑扑动力学的中型无人驾驶直升机的姿态和高度控制。建立了简化的UAH模型,并设计了非线性干扰观测器(NDO)以消除未知外部干扰的影响。鲁棒的自适应反推方法用于为跟踪期望轨迹的输出设计姿态和高度控制器。通过Lyapunov分析证明了闭环系统的稳定性,并且所有闭环信号最终均一地有界。仿真结果表明了所开发控制方法的有效性。

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