BTT导弹总体设计中气动特性与控制系统的协调分析

AN INTEGRATED ANALYSIS OF AERODYNAMIC CONFIGURATION AND CONTROL SYSTEM IN DESIGN OF BTT MISSILE

从协调控制对导弹气动外形的要求出发,讨论了BTT导弹的动力学特性及其控制系统的特点。分析了无耦合扰动运动及耦合对导弹的稳定性和操纵性的影响,并从导弹总体设计的角度提出了BTT导弹自动驾驶仪的设计要求及导弹稳定性、操纵性等参数的选择方法。

Based on aerodynamic configuration requirements for Coordinated BTT missile control system. missile-body dynamic model and characteristics of control system are discussed, Uncoupled disturbed motion as well as the effect of coupling on stability and controllability of missile are analysed. From the point of view of system de sign, demands for designing autopilot and principle selecting stability and controllability parameter for BTT missile are presented.