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Hierarchy robust control for unmanned quadrotor helicopter without linear velocity measurement

机译:无线速度直升机的无人四旋翼直升机层次鲁棒控制

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摘要

Considering the parameter measurement errors of a low-cost quadrotor system and the constant wind disturbance during flight, a hierarchy robust control strategy for unmanned quadrotor helicopter is constructed. The hierarchy robust control strategy is that the attitude and position loops of the quadrotor adopt different robust control strategy. The integral backstepping controller is applied to stabilise the attitude angles of the quadrotor with parameter errors. The linear robust controller with a compensator for the constant wind is applied to fulfil the position tracking. Sliding mode observer for the quadrotor position subsystem is founded to estimate the linear velocity when the direct measurement is unavailable. The simulating test is implemented and the simulation test results show that the control algorithm is stable and can effectively reject the constant wind disturbance and have strong robustness to the parameter errors.
机译:考虑到低成本四旋翼系统的参数测量误差和飞行过程中的恒定风扰,构造了无人四旋翼直升机的分级鲁棒控制策略。层次鲁棒控制策略是四旋翼的姿态和位置环采用不同的鲁棒控制策略。积分反步控制器用于稳定具有参数误差的四旋翼的姿态角。采用带有恒定风量补偿器的线性鲁棒控制器来完成位置跟踪。建立了四旋翼位置子系统的滑模观测器,以在无法进行直接测量时估算线速度。进行了仿真测试,仿真结果表明,该控制算法稳定,可以有效抑制恒定风干扰,对参数误差具有很强的鲁棒性。

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