航空兵器Issue(4)：15-19,24,6.
高速飞行器直接力／气动力复合控制技术综述
Survey of Compound Control Methods of Reaction Thrust and Aerodynamic Fin of Flight Vehicle
摘要
Abstract
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 .关键词
高速飞行器/拦截器/复合控制/控制系统设计Key words
high-velocity vehicle/interceptor/compound control/control system design分类
军事科技引用本文复制引用
梁栋,宋建梅,蔡高华..高速飞行器直接力／气动力复合控制技术综述[J].航空兵器,2013,(4):15-19,24,6.基金项目
航空科学基金（20110172001）；北京理工大学科技创新计划重大项目培育专项计划（2011 CX01007）资助 （）
