可重构无人飞艇多体建模与自适应控制

Gilmar Tuta-Navajas, E. Lanteigne
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引用次数: 1

摘要

本文介绍了利用重心变化控制无人飞艇俯仰的方法。重心的变化是通过控制一个可移动的贡多拉沿着固定在氦气包层的弓的刚性龙骨的位置来实现的。利用测量和估计的物理特性建立了纵向多体运动方程,并设计了自适应PID控制器来控制俯仰角。在一艘4米长的无人飞艇样机上进行了飞行试验,验证了该方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Multi-body modelling and adaptive control of a re-configurable uninhabited airship
This paper presents pitch control of an uninhabited airship using changes in center of gravity. Changes in center of gravity are achieved by controlling the position of a movable gondola along a rigid keel fixed to the bow of the helium envelope. The longitudinal multi-body dynamic equations of motion were developed using the measured and estimated physical properties and an adaptive PID controller was designed to control the pitch angle. Flight tests on a 4 m long uninhabited airship prototype were conducted to demonstrate the effectiveness of the method.
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