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带推力矢量飞机的重构飞控系统设计
引用本文:苏浩秦,邓建华.带推力矢量飞机的重构飞控系统设计[J].飞行力学,2002,20(4):27-30.
作者姓名:苏浩秦  邓建华
作者单位:西北工业大学,飞机系,陕西,西安,710072
摘    要:带推力矢量飞机的重构飞行控制系统是由带推力知量的基本飞行控制系统和重构控制系统两部分组成。前者是加装推力矢量飞机控制的关键。后者是当飞机舵面或作动器发生故障后,利用矢量喷管进行飞控敏理构,可以使推力矢量再次发挥作用。以加装推力矢量喷管的飞机为研究对象,阐述了上述两种控制系统的详细设计方法,此法带有一定的普遍性,为进一步展开这方面的研究提供了参考。

关 键 词:推力矢量  飞机  设计  飞行控制  气动性能
文章编号:1002-0853(2002)04-0027-04
修稿时间:2002年2月1日

Reconfigurable Control System Design for the Aircraft Mounted Thrust Vector
SU Hao-qin,DENG Jian-hua.Reconfigurable Control System Design for the Aircraft Mounted Thrust Vector[J].Flight Dynamics,2002,20(4):27-30.
Authors:SU Hao-qin  DENG Jian-hua
Abstract:It's one key method for aircraft mounted the thrust vector engine that its flight control system is redesigned, also when actuators are failure, how to make use of the thrust vector to get the reconfigurable fly system is another key design method. The paper illustrates the above two methods which are based on the aircraft mounted the thrust vector engine, however the material useful design methods are proposed for the idiographic design.
Keywords:thrust vector  reconfigurable flight control system  aircraft failure
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