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A Liouvillian systems approach for the trajectory planning-based control of helicopter models

机译:基于轨迹规划的直升机模型控制的Liouvillian系统方法

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摘要

A feedback regulation scheme, based on off-line trajectory planning and an approximate state linearization, is proposed for the hover-to-hover stabilization of simplified, underactuated, models of a helicopter system. The approach, based on the 'Liouvillian' character of the helicopter kinematic equations, advantageously uses the total, or partial, differential flatness property of the system models. The controller performance is evaluated through digital computer simulations which include initial state setting errors of significant magnitudes. Copyright (C) 2000 John Wiley & Sons, Ltd. [References: 19]
机译:提出了一种基于离线轨迹规划和近似状态线性化的反馈调节方案,用于简化,欠驱动的直升机系统模型的悬停到悬停稳定。该方法基于直升机运动方程的“ Liouvillian”特征,有利地使用了系统模型的全部或部分微分平坦度特性。控制器的性能通过数字计算机仿真来评估,其中包括大量初始状态设置误差。版权所有(C)2000 John Wiley&Sons,Ltd. [参考:19]

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