直接力/气动力复合控制技术发展综述  

Review on Development of Direct Force/Aerodynamic Force Compound Control Technology

作　　者：郭建国[1] 彭谦 周敏[1] Guo Jianguo;Peng Qian;Zhou Min(Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学精确制导与控制研究所,西安710072

出　　处：《航空兵器》2022年第1期1-13,共13页Aero Weaponry

基　　金：国家自然科学基金项目(61973254,62003270)。

摘　　要：直接力/气动力复合控制的本质是利用直接力响应速度快的特性提升被控飞行器的机动性和快速性,能够有效补偿气动力不足导致的气动力控制响应慢问题。本文阐述了直接力/气动力复合控制系统的特性及关键问题,从发动机配置方式、国内外直接力建模研究现状、以及直接力控制干扰建模三方面介绍了直接力/气动力复合控制系统建模方法,从控制方式、国内外直接力/气动力复合控制研究现状、以及脉冲发动机点火算法三方面介绍了直接力/气动力复合控制方法,给出了可行的发动机复合系统稳定性分析方法,对直接力/气动力复合控制未来的发展趋势进行了展望,并对其关键技术进行了总结。The essence of direct force/aerodynamic force compound control is to improve the maneuverability and rapidity of controlled aircraft by using the fast response speed of direct force,which can effectively compensate the slow response of aerodynamic control caused by insufficient aerodynamic force.This paper describes the characteristics and key problems of direct force/aerodynamic force compound control system,and introduces the modeling method of direct force/aerodynamic force compound control system from three aspects:the configuration of engine,the existing research of direct force modeling at home and abroad,and the disturbance modeling of direct force control.The direct force/aerodynamic force compound control method is introduced from three aspects:the control method,the existing research of direct force/aerodynamic force compound control method at home and abroad,and the ignition algorithm of pulse engine.The feasible direct force/aerodynamic force compound system stability analysis method is given,the future development trend of direct force/aerodynamic force compound control is prospected,and its key technologies are summarized.

关 键 词：直接力 气动力 制导控制系统 直接侧向力 控制分配 脉冲发动机 点火算法 

分 类 号：TJ760[兵器科学与技术—武器系统与运用工程] V249.1[航空宇航科学与技术—飞行器设计]