摘要
The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
| 编辑 | Shengyuan Xu, Qianchuan Zhao |
| 出版商 | IEEE Computer Society |
| 页 | 960-965 |
| 页数 | 6 |
| ISBN（电子版） | 9789881563842 |
| DOI | |
| 出版状态 | 已出版 - 11 9月 2014 |
| 活动 | Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, 中国 期限: 28 7月 2014 → 30 7月 2014 |
出版系列
| 姓名 | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
|---|---|
| ISSN（印刷版） | 1934-1768 |
| ISSN（电子版） | 2161-2927 |
会议
| 会议 | Proceedings of the 33rd Chinese Control Conference, CCC 2014 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Nanjing |
| 时期 | 28/07/14 → 30/07/14 |
指纹
探究 'Adaptive sliding mode control for missile guidance law' 的科研主题。它们共同构成独一无二的指纹。引用此
Wu, X., Bi, S., Zhu, Z., & Wu, W. (2014). Adaptive sliding mode control for missile guidance law. 在 S. Xu, & Q. Zhao (编辑), Proceedings of the 33rd Chinese Control Conference, CCC 2014 (页码 960-965). 文章 6896757 (Proceedings of the 33rd Chinese Control Conference, CCC 2014). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2014.6896757