| 战术导弹的鲁棒自校正制导及单片机实现 |
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| 引用本文： | 张志勇,康景利.战术导弹的鲁棒自校正制导及单片机实现[J].宇航学报,1992(3):13-18. |
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| 作者姓名： | 张志勇 康景利 |
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| 作者单位： | 清华大学，清华大学，清华大学，北京理工大学 北京，北京，北京 |
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| 摘 要： |
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| 关 键 词： | 制导 时变参数 辨识 战术导弹 鲁棒 |
ROBUST SELF-TUNING GUIDANCE LAW FOR TACTICAL MISSILE AND ITS REALIZATION WITH SINGLE-CHIP MICROCOMPUTER |
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| Zhang Zhiyong Wang Shimi Fang Chongzhi.ROBUST SELF-TUNING GUIDANCE LAW FOR TACTICAL MISSILE AND ITS REALIZATION WITH SINGLE-CHIP MICROCOMPUTER[J].Journal of Astronautics,1992(3):13-18. |
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| Authors: | Zhang Zhiyong Wang Shimi Fang Chongzhi |
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| Institution: | Zhang Zhiyong Wang Shimi Fang Chongzhi (Tsinghua University)Kang Jingli (Beijing Intitnte of Technology) |
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| Abstract: | This paper presents a new guidance law-robust self-tuning guidance law(RSTGL). In the RSTGL, the nigh order and nonlinear complex model of a tactical missile is equivalent to reduced-order and linear time-varying models. The identification algorithm for time-varying parameters and robust self-tuning guidance algorithm are proposed based on tnis equivalent reduced-order model. Simulation experiments have proved that the RSTGL has high hitting accuracy and aisturbance rejection ability. Especially, because of its simple structure, the RSTGL is easy to be implemented in engineering. Tnis paper also discusses some problems in the guidance system realization with single-chip microcomputer. |
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| Keywords: | Guidance Time-varying parameters Identification Self-tuning |
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