[1]时宏钢,王俊鹍,吕长起,等.战术导弹变结构自适变自动驾驶仪研究[J].郑州大学学报(工学版),1992,13(02):71-76.
　Shi Honggang,Wang Junyi,Lu Changqi,et al.Research on the Research on Tactical Missile Change Structure Autonomous Driving Instrument Research[J].Journal of Zhengzhou University (Engineering Science),1992,13(02):71-76.
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战术导弹变结构自适变自动驾驶仪研究()
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《郑州大学学报(工学版)》[ISSN:1671-6833/CN:41-1339/T]

卷:
13卷
期数:
1992年02期
页码:
71-76
栏目:
出版日期:
1992-06-28

文章信息/Info

Title:
Research on the Research on Tactical Missile Change Structure Autonomous Driving Instrument Research
作者:
时宏钢;王俊鹍;吕长起;
郑州工学院,航空航天部014中心,航空航天部014中心,
Author(s):
Shi Honggang; Wang Junyi; Lu Changqi;
Zhengzhou Institute of Technology, Center 014 Center, Ministry of Aerospace Ministry 014 Center,
关键词:
自动驾驶仪; 自适应控制; 变结构系统
Keywords:
Autonomous driving instrument;  adaptive control;  change structural system
文献标志码:
A
摘要:
本文针对战术导弹古典自动驾驶仪的缺点,利用变结构控制理论、吸取模型参考控制的优点并引入趋近律,设计出具有趋近律的模型参考变结构自适应自动驾驶仪.该自适应自动驾驶仪的性能较为令人满意.
Abstract:
For the shortcomings of the classical self -driving instrument of tactical missiles, use the advantages of changing structural control theory, absorbing model reference control, and introducing approaching the law. Design a model reference for the desertation structure of the model of the law.

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更新日期/Last Update: 1900-01-01