| BTT导弹协调式耦合变结构自动驾驶仪设计 |
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| 引用本文： | 朱志刚,杨文利.BTT导弹协调式耦合变结构自动驾驶仪设计[J].宇航学报,1997,18(1):8-12. |
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| 作者姓名： | 朱志刚 杨文利 |
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| 作者单位： | [1]北京142信箱403分箱 [2]西安电力机械制造公司 |
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| 摘 要： | 本文应用多变量不确定性系统的模型参考变结构自适应控制理论设计了某型ＢＴＴ导弹协调中变结构自动驾驶仪，有铲地克服了通道间的交叉耦合效应，较好地保证了ＢＴＴ导弹偏航衮动通道之间的协调动作，获得了较高的指令跟踪性能。
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| 关 键 词： | BTT 导弹 自动驾驶仪 变结构 |
DESIGN OF BTT MISSILE COORDINATED COUPLE VARIABLE STRUCTURE AUTOPILOT |
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| Zhu Zhigang.DESIGN OF BTT MISSILE COORDINATED COUPLE VARIABLE STRUCTURE AUTOPILOT[J].Journal of Astronautics,1997,18(1):8-12. |
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| Authors: | Zhu Zhigang |
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| Institution: | Zhu Zhigang (Beijing Control Device Institute) Yang Wenli (Xi'an Electrical Equipment Manufacturing Corporation) |
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| Abstract: | The Bank to Turn (BTT) missile coordinated couple variable structure autopilot,which is designed by model reference variable structure adaptive control theory for multivariable uncertain system,efficiently overcomes the cross coupled influence among three channels,guarantees the coordination between BTT missile's yaw channel and roll channel,and obtains the satisfactory instruction following performance |
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| Keywords: | BTT missile Autopilot Variable Structure Model Reference |
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