| BTT导弹利亚普诺夫制导律的工程应用 |
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| 引用本文： | 张飞宇.BTT导弹利亚普诺夫制导律的工程应用[J].弹道学报,2011,23(1):80-83. |
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| 作者姓名： | 张飞宇 |
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| 作者单位： | 北京理工大学宇航科学技术学院,北京,100081 |
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| 摘 要： | 为了解决BTT导弹制导的传统难题,将利亚普诺夫方法引入BTT导弹制导律的设计中,得到卡尔曼滤波器结构,形成BTT导弹利亚普诺夫制导系统,分析了反正切方法形成的BTT导弹比例导引(PN)系统与BTT导弹增强型比例导引(APN)系统,得到了考虑驾驶仪滞后、过栽为0时奇点限制的具有更优制导性能的BTT导弹利亚普诺夫制导律.对...
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| 关 键 词： | 制导律 比例导引 卡尔曼滤波器 BTT导弹 |
Engineering Application of Lyapunov Guidance Law on Bank-to-Turn Missile |
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| ZHANG Fei-yu.Engineering Application of Lyapunov Guidance Law on Bank-to-Turn Missile[J].Journal of Ballistics,2011,23(1):80-83. |
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| Authors: | ZHANG Fei-yu |
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| Affiliation: | ZHANG Fei-yu(School of Aerospace Science and Engineering,BIT,Beijing 100081,China) |
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| Abstract: | In order to resolve the traditional problem of BTT missile guidance law,the Lyapunov stability theory was introduced to design BTT missile guidance law.The structure of Kalman filter was obtained,and the Lyapunov guidance system was realized.Proportional navigation(PN)law and augmented proptional narigation(APN)law of BTT missile were formed by applying the arctangent function,and the three BTT laws were analyzed and compared.BTT Lyapunov guidance law considering the autopilot lag effect and singularity lim... |
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| Keywords: | guidance law proportional navigation Kalman filter bank-to-turn missile |
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