摘要
介绍了过失速机动战斗机飞行控制系统的结构及控制律的设计方法，并对控制中各回路增益的计算做了详细的描述。此外，还论述了推力矢量（ＴＶ，ＴｈｒｕｓｔＶｅｃｔｏｒｉｎｇ）控制与气动操纵面的协调操纵等问题。通过分析与研究，总结出飞行控制律设计的几个关键问题，为从事推力矢量研究的科技人员提供了参考。
This paper introduces the configuration of flight control system and thedesign philosophy of flight control law. Moreover, the gain calculation of the flight control law paths are presented. The coordination method between thrust vectoring controland aerodynamic control follow. Through analysing and researching, some importantconclusions are obtained. These conclusions can provide references for technicians whoare engaged in thrust vectoring research.
出处
《飞行力学》
CSCD
北大核心
1996年第2期42-47,共6页
Flight Dynamics
