摘要
The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011 |
| 页 | 507-514 |
| 页数 | 8 |
| DOI | |
| 出版状态 | 已出版 - 2011 |
| 活动 | 2011 International Conference on Automation and Robotics, ICAR 2011 - Dubai, 阿拉伯联合酋长国 期限: 1 12月 2011 → 2 12月 2011 |
出版系列
| 姓名 | Lecture Notes in Electrical Engineering |
|---|---|
| 卷 | 123 LNEE |
| ISSN（印刷版） | 1876-1100 |
| ISSN（电子版） | 1876-1119 |
会议
| 会议 | 2011 International Conference on Automation and Robotics, ICAR 2011 |
|---|---|
| 国家/地区 | 阿拉伯联合酋长国 |
| 市 | Dubai |
| 时期 | 1/12/11 → 2/12/11 |
指纹
探究 'Analysis for height control-loop of cruise missile to different kinds of autopilot' 的科研主题。它们共同构成独一无二的指纹。引用此
Wen, Q., Xia, Q., & Cai, C. (2011). Analysis for height control-loop of cruise missile to different kinds of autopilot. 在 Advances in Automation and Robotics, Vol. 2 - Selected Papers from the 2011 International Conference on Automation and Robotics, ICAR 2011 (页码 507-514). (Lecture Notes in Electrical Engineering; 卷 123 LNEE). https://doi.org/10.1007/978-3-642-25646-2_66