| BTT导弹总体设计中气动特性与控制系统的协调分析 |
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| 引用本文： | 高鹏飞.BTT导弹总体设计中气动特性与控制系统的协调分析[J].战术导弹技术,1993(2):15-21,9. |
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| 作者姓名： | 高鹏飞 |
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| 作者单位： | 北京航空航天大学 |
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| 摘 要： | 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。
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| 关 键 词： | 导弹 动力学模型 控制系统 |
AN INTEGRATED ANALYSIS OF AERODYNAMIC CONFIGURATION AND CONTROL SYSTEM IN DESIGN OF BTT MISSILE |
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| Gao Pengfei Beijing University of Aeronautics and Astronautics.AN INTEGRATED ANALYSIS OF AERODYNAMIC CONFIGURATION AND CONTROL SYSTEM IN DESIGN OF BTT MISSILE[J].Tactical Missile Technology,1993(2):15-21,9. |
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| Authors: | Gao Pengfei Beijing University of Aeronautics and Astronautics |
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| Affiliation: | Gao Pengfei Beijing University of Aeronautics and Astronautics |
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| Abstract: | 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. |
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| Keywords: | BTT missile Dynarmic model Control system Coupling Disturbance |
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