| BTT导弹时变滑态变结构自适应自动驾驶仪设计 |
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| 引用本文： | 张科,常新杰,周凤歧.BTT导弹时变滑态变结构自适应自动驾驶仪设计[J].航天控制,1999(4). |
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| 作者姓名： | 张科 常新杰 周凤歧 |
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| 作者单位： | 西北工业大学航天学院!西安710072 |
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| 摘 要： | 针对倾斜转弯导弹的具体特点, 提出了一种基于模型参考时变全程滑态变结构控制理论的协调式耦合自动驾驶仪的设计方法, 并分别针对滚转通道、俯仰/偏航耦合通道进行了设计分析; 最后进行了三通道联合仿真, 得到了满意的结果
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| 关 键 词： | 倾斜转弯技术 变结构控制 自动驾驶仪 导弹 |
On Design of Time-Varying Sliding-Mode Variable Structure\;Adaptive Control for BTT Missile Autopilot |
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| Zhang Ke Chang Xinjie Zhou Fengqi Northwestern Polytechnical University,Xi'an.On Design of Time-Varying Sliding-Mode Variable Structure\;Adaptive Control for BTT Missile Autopilot[J].Aerospace Control,1999(4). |
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| Authors: | Zhang Ke Chang Xinjie Zhou Fengqi Northwestern Polytechnical University Xi'an |
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| Institution: | Zhang Ke Chang Xinjie Zhou Fengqi Northwestern Polytechnical University,Xi'an 710072 |
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| Abstract: | Based on the time-varying sliding-mode variable structure adaptive control theories, a new coordinate coupling autopilot design scheme for BTT missiles is proposed. Design for roll channel and pitch/yaw coupling channel is also analised respectivly. Finally, the outstanding feature of our design is proved by digital simulations results. |
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