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无人机横侧向飞行控制系统研究
引用本文:席庆彪,袁冬莉,闫建国.无人机横侧向飞行控制系统研究[J].飞行力学,2004,22(4):16-18.
作者姓名:席庆彪  袁冬莉  闫建国
作者单位:1. 西北工业大学,无人机研究与发展中心,陕西,西安,710072
2. 西北工业大学,自动化学院,陕西,西安,710072
基金项目:863计划资助项目(2002AA755022)
摘    要:采用非相似余度设计思想,建立了无人机横侧向控制系统.对典型故障模式的控制系统进行了分析,结果表明该系统不但具有较好的控制品质,而且对单通道控制故障引起的干扰具有较好的抑制能力,可有效解决副翼故障可能导致的飞行事故问题,从而提高系统的可靠性.

关 键 词:无人机  非相似余度设计  飞行控制
文章编号:1002-0853(2004)04-0016-03
修稿时间:2003年11月18

A Study of Lateral Flight Control System of UAV
XI Qing-biao,YUAN Dong-li,YAN Jian-guo.A Study of Lateral Flight Control System of UAV[J].Flight Dynamics,2004,22(4):16-18.
Authors:XI Qing-biao  YUAN Dong-li  YAN Jian-guo
Institution:XI Qing-biao~1,YUAN Dong-li~2,YAN Jian-guo~2
Abstract:Using the traditional coordination control configure for UAV, it is inadequate by closing an aileron channel in order to get rid of flying security-hidden trouble caused by a fault aileron. At the same time the lateral-direction control is unstable. With the method of dissimilar redundant design, this paper put forwards a lateral direction control system of UAV. From simulation results, this system not only has fine flight control qualities but also has good ability to restrain the disturbance caused by a single channel. This system can solve the flying accident when an aileron channel is in trouble, furthermore it can improve the reliability and security of the flight system.
Keywords:unmanned aerial vehicle  dissimilar redundant design  flight control
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