| 基于副翼效率C_3辨识的导弹自动驾驶仪设计 |
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| 引用本文： | 陈星阳,朱楠,张辉.基于副翼效率C_3辨识的导弹自动驾驶仪设计[J].情报指挥控制系统与仿真技术,2011(2):87-89. |
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| 作者姓名： | 陈星阳 朱楠 张辉 |
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| 作者单位： | 中国空空导弹研究院,河南洛阳471009 |
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| 摘 要： | 在无法得知导弹飞行高度和速度的情况下,所设计的导弹自动驾驶仪增益难以满足全空域飞行的需要。本文采用一种基于横滚通道副翼效率C3辨识的自动驾驶仪增益设计方法,利用此方法设计的自动驾驶仪增益能够满足导弹全空域飞行的需要。
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| 关 键 词： | 自动驾驶仪增益 横滚通道 副翼效率 |
Missile Autopilot Design Based on Aileron Efficiency C_3 Identification |
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| CHEN Xing-yang,ZHU Nan,ZHANG Hui.Missile Autopilot Design Based on Aileron Efficiency C_3 Identification[J].Information Command Control System and Simulation Technology,2011(2):87-89. |
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| Authors: | CHEN Xing-yang ZHU Nan ZHANG Hui |
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| Institution: | (China Airborne Missile Academy,Luoyang 471009,China) |
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| Abstract: | It is difficult to satisfy all-airspace flight with missile autopilot gains,which are designed without flying height and velocity.In this paper,a method of autopilot gain design based on roll channel fin effectiveness C3 identification is introduced.With this method,we can design the appropriate autopilot gains for missile all-airspace flight. |
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| Keywords: | autopilot gains roll channel fin effectiveness |
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