| 一类导弹控制系统的模态解耦 |
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| 引用本文： | 姜玉宪.一类导弹控制系统的模态解耦[J].宇航学报,1987(3). |
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| 作者姓名： | 姜玉宪 |
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| 作者单位： | 北京航空学院 |
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| 摘 要： | 本文研究非旋转式导弹控制系统的模态解耦能力。证明了具有俯仰、偏航和滚动三个控制通道的控制系统可以实现俯仰、偏航两种运动模态对滚动运动模态的完全解耦。给出了模态解耦控制系统的设计方法。对一种导弹控制系统进行了验证性设计,做了数字仿真。
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| 关 键 词： | 控制系统 导弹 去耦 横向控制 数字模拟 |
DECOUPLING OF A KIND OF MISSILE CONTROL SYSTEM MODES |
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| Jiang Yuxian.DECOUPLING OF A KIND OF MISSILE CONTROL SYSTEM MODES[J].Journal of Astronautics,1987(3). |
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| Authors: | Jiang Yuxian |
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| Institution: | Beijing Institute of Aeronautics and Astronautics |
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| Abstract: | The ability of modes decoupling about control system of un-rotating missile was studied. It was verified that the full-decoupling of modes effected by pitch and yaw to roll can be realized for the control system in which there are pitch, yaw and roll three control channels. An approach for designing the control system in which the couplings between modes were canceled was presented. A demonstrating example for designing missile attitude control system was carried out, and the dynamical simulation of this control system was made. |
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| Keywords: | Control system Guided missile Decoupling Lateral control Digital simulation |
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