高速飞行器直接力／气动力复合控制技术综述

摘要

直接力/气动力复合控制技术是实现高速飞行器大机动、快响应和高精度飞行的有效手段。本文介绍了国外几种高速飞行器的复合控制模式及系统组成，并对国内外直接力/气动力复合控制系统的主要设计方法和研究进展进行了分析总结，指出了基于分配的设计方法及联合设计方法的优缺点及进一步研究中要注意的问题。%The compound control system method of the reaction thrust and aerodynamic fin will be the main and key technology to implement the high-maneuver , fast response , and high-accuracy for hy-personic flight vehicle .This paper introduces some compound control modes and system construction of some high-velocity flight vehicles in abroad , and analyzes the development of the compound control system design methods of the reaction thrust and aerodynamic fin in detail .The paper presents some merits and flaws of distribution-based design method and joint-design method , and some cautions during further re-searoh .