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On the regulation of a helicopter system: A trajectory planning approach for the Liouvillian model

机译:关于直升机系统的管制:Liouvillian模型的轨迹规划方法

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A feedback regulation scheme is presented which allows for a wide range of displacement maneuvers on a simplified longitudinal model of a helicopter system which is underactuated and nondifferentially flat. The system, nevertheless, is shown to be of the "Liouvillian" type. An off-line, open loop, trajectory planning procedure is proposed, based on the solution of differential equations for the desired attitude angle reference signal, which precisely results in the desired nominal horizontal displacement trajectory. The performance of a proposed feedback controller, which exploits the fact that the linearized system has its coefficients on a Hardy filed, is evaluated through digital computer simulations including unmodelled mid course wind gusts and initial setting errors.
机译:提出了一种反馈调节方案,该方案允许在直升机系统的简化纵向模型上进行大范围的位移操纵,该直升机模型驱动不足且无差速。但是,该系统显示为“ Liouvillian”类型。基于所需姿态角参考信号的微分方程的解,提出了一种离线,开环的轨迹规划程序,该程序精确地导致了所需的名义水平位移轨迹。通过数字计算机模拟(包括未建模的中风和初始设置误差)评估了所提出的反馈控制器的性能,该控制器利用了线性化系统将其系数保存在Hardy字段上的事实。

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