摘要
The design for missile integrated guidance control is to combine the missile guidance and control circuit into one loop. According to the relative motion of the missile and target, the control command is directly obtained to further improve the guidance and control precision. This paper summarizes the domestic and foreign research progress on the design methods of missile integrated guidance control in recent years, studies and summarizes its advantages and disadvantages, and analyzes the main problems and development trend of missile integrated guidance and control design.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | 2017 International Conference on Automation, Control and Robots, ICACR 2017 |
| 出版商 | Association for Computing Machinery |
| 页 | 15-19 |
| 页数 | 5 |
| ISBN（电子版） | 9781450363501 |
| DOI | |
| 出版状态 | 已出版 - 22 12月 2017 |
| 活动 | 2017 International Conference on Automation, Control and Robots, ICACR 2017 - Wuhan, 中国 期限: 22 12月 2017 → 24 12月 2017 |
出版系列
| 姓名 | ACM International Conference Proceeding Series |
|---|
会议
| 会议 | 2017 International Conference on Automation, Control and Robots, ICACR 2017 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Wuhan |
| 时期 | 22/12/17 → 24/12/17 |
指纹
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Fu, Z., Dai, Y., & Zhang, K. (2017). Research progress on design methods for missile integrated guidance and control. 在 2017 International Conference on Automation, Control and Robots, ICACR 2017 (页码 15-19). (ACM International Conference Proceeding Series). Association for Computing Machinery. https://doi.org/10.1145/3175516.3175524