摘要
带推力矢量飞机的重构飞行控制系统是由带推力矢量的基本飞行控制系统和重构控制系统两部分组成的。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系统重构 ,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。
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.
出处
《飞行力学》
CSCD
2002年第4期27-30,共4页
Flight Dynamics
关键词
推力矢量
飞机
设计
飞行控制
气动性能
thrust vector
reconfigurable flight control system
aircraft failure
