摘要
The purpose of this research is to propose a rapid design of guidance and control loop for laser guided bomb. Aerodynamic parameters which are difficult to obtain fast at the beginning of design, are calculated by Missile Datcom software. Then every parameter of missile body transfer function is achieved and precious transfer function is determined. Furthermore, pitching stability loop, side stability loop, roll stability loop and gravity compensation loop are built. Then all the designed loops and target practice are simulated in Matlab/Simulink, and the results demonstrate that the design is correct and effective.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Proceedings of the 32nd Chinese Control Conference, CCC 2013 |
| 出版商 | IEEE Computer Society |
| 页 | 5620-5625 |
| 页数 | 6 |
| ISBN（印刷版） | 9789881563835 |
| 出版状态 | 已出版 - 18 10月 2013 |
| 活动 | 32nd Chinese Control Conference, CCC 2013 - Xi'an, 中国 期限: 26 7月 2013 → 28 7月 2013 |
出版系列
| 姓名 | Chinese Control Conference, CCC |
|---|---|
| ISSN（印刷版） | 1934-1768 |
| ISSN（电子版） | 2161-2927 |
会议
| 会议 | 32nd Chinese Control Conference, CCC 2013 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Xi'an |
| 时期 | 26/07/13 → 28/07/13 |
指纹
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Li, M., Yin, J., Wang, J., & Xu, J. (2013). Rapid design of guidance and control loop for laser guided bomb. 在 Proceedings of the 32nd Chinese Control Conference, CCC 2013 (页码 5620-5625). 文章 6640420 (Chinese Control Conference, CCC). IEEE Computer Society.