摘要
To improve accuracy of artillery rocket is a crucial problem especially for long-range multiple launch rocket system. A kind of simplified control system can control the rocket during boost phase, but cannot compensate for disturbance during coast phase. In this paper, a guidance and control system making use of low cost IMU/GPS (Inertial Measurement Unit/Global Positioning System) is introduced, by which disturbance during both phase can be restricted. Guidance adds extra cost to the rocket but is more than offset by increased effectiveness.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Proceedings of the International Symposium on Test and Measurement |
| 页 | 93-95 |
| 页数 | 3 |
| 出版状态 | 已出版 - 2003 |
出版系列
| 姓名 | Proceedings of the International Symposium on Test and Measurement |
|---|---|
| 卷 | 1 |
指纹
探究 'Guidance and Control System Making Use of Low Cost IMU/GPS for Guided Artillery Rocket' 的科研主题。它们共同构成独一无二的指纹。引用此
She, H., & Yang, S. (2003). Guidance and Control System Making Use of Low Cost IMU/GPS for Guided Artillery Rocket. 在 Proceedings of the International Symposium on Test and Measurement (页码 93-95). (Proceedings of the International Symposium on Test and Measurement; 卷 1).