| 倾斜转弯导弹耦合通道控制研究 |
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| 引用本文： | 周军,周凤岐.倾斜转弯导弹耦合通道控制研究[J].航天控制,1997(3). |
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| 作者姓名： | 周军 周凤岐 |
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| 作者单位： | 西北工业大学航天工程学院!西安，710072，西北工业大学航天工程学院!西安，710072 |
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| 摘 要： | 倾斜转弯（BTT）导弹的俯仰与偏航通道之间存在着强烈耦合，使得根据经典控制理论的自动驾驶仪三通道独立设计方法遇到一定困难。基于局部模型跟踪理论，研究了倾斜转弯导弹的耦合控制问题，提出了一种新的自动驾驶仪设计方法，该方法能有效地提高导弹控制精度和快速响应能力。
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| 关 键 词： | 自动驾驶仪 俯仰 偏航 变量 控制 |
Research on Couping Channel Control of the Bank-to-Turn Missile |
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| Zhou Jun, Zhou Fengqi.Research on Couping Channel Control of the Bank-to-Turn Missile[J].Aerospace Control,1997(3). |
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| Authors: | Zhou Jun Zhou Fengqi |
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| Abstract: | Strong coupling is in existence between pitch and yaw channel of the bank-to-turn (BTT) missile, it makes that autopilot three-channel independent design method according to clasical control theory involves certain difficulties. Based on partial model follwwing control theory, coupling control problem of the bank - to - turn misile is studied and a new design method of autopilot is presented in this paper. This method can effectively improve control accurcy and high - speed response ability of the missile. |
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| Keywords: | Autopilot Pitch Yaw Variable Control |
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