| 引用本文: | 张嗣瀛.一个控制系统的解耦问题[J].控制理论与应用,1984,1(2):3~10.[点击复制] |
| Zhang Siying.THE DECOUPLING PROBLEM OF A CONTROL SYSTEM[J].Control Theory and Technology,1984,1(2):3~10.[点击复制] |
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| 一个控制系统的解耦问题 |
| THE DECOUPLING PROBLEM OF A CONTROL SYSTEM |
| 摘要点击 994 全文点击 591 投稿时间：1983-02-19 修订日期：1983-05-05 |
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| DOI编号 |
| 1984,1(2):3-10 |
| 中文关键词 |
| 英文关键词 |
| 基金项目 |
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| 中文摘要 |
| 一导弹在飞行中同时绕其纵轴旋转，控制系统将操纵它的俯仰和偏航两种运动。但若有关参数选择不当，将产生交叉耦合现象，即当给出俯仰指令时却同时产生偏航运动，反之亦然。本文给出一种解耦方法。 |
| 英文摘要 |
| When a controlled rocket is rotating around its longitudinal axis in flying, the control system manoeuvres its pitching and crabbing movement. If the relevant parameters are unsuitably selected, the cross coupling problem will arise, i.e., when giving a pitching control command, some crabbing motion will follow and vice versa. In this paper, a decoupling method is presented. |
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