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Three-loop Feedback Anti-wind Disturbance Control for The VTOL Aircraft without Vector Thrust

机译:无矢量推力的垂直起降飞机的三环反馈抗风扰动控制

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The vertical takeoff and landing (VTOL) aircraft without vector thrust can only generate lateral force through attitude adjustment in the takeoff and landing phase. It cannot change the thrust vector to resist lateral wind disturbance. Therefore, its ability of the anti-wind disturbance is weak. For this reason, a new type of anti-wind disturbance control strategy is proposed in this paper. An intermediate loop fed back by the wind disturbance estimator is introduced between the outer loop of position feedback and the inner loop of attitude feedback. The estimation of disturbance acceleration fed back by the intermediate loop corrects the position control command of outer loop feedback so that the thrust control can achieve suppression of the tangential wind disturbance and the inner loop of attitude control can achieve suppression of the lateral wind disturbance. The simulation results show that control strategy proposed in this paper can well estimate and compensate external wind disturbance received by the system.
机译:没有矢量推力的垂直起降(VTOL)飞机只能通过在起降阶段的姿态调整来产生侧向力。它不能更改推力矢量以抵抗横向风干扰。因此,其抗风干扰能力较弱。为此,本文提出了一种新型的防风扰动控制策略。在位置反馈的外环和姿态反馈的内环之间引入一个由风扰估计器反馈的中间环。中间回路反馈的干扰加速度的估计值校正了外部回路反馈的位置控制命令,从而推力控制可以实现切向风扰动的抑制,姿态控制的内部回路可以实现侧风扰动的抑制。仿真结果表明,本文提出的控制策略可以很好地估计和补偿系统接收到的外部风扰。

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