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

H. Sira-Ramírez, R. Castro-Linares
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引用次数: 6

Abstract

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.
直升机系统的调节:Liouvillian模型的轨迹规划方法
针对欠驱动、无差平的直升机系统纵向简化模型,提出了一种允许大范围位移机动的反馈调节方案。然而,该系统显示为“Liouvillian”类型。在解姿态角参考信号微分方程的基础上,提出了一种离线开环弹道规划方法,该方法可以精确地得到期望的标称水平位移轨迹。利用线性化系统在Hardy场上具有其系数的事实,所提出的反馈控制器的性能通过数字计算机模拟进行评估,包括未建模的中途阵风和初始设置误差。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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