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浏览/检索结果: 共5条，第1-5条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 A Novel LOS Rate Estimation Method Based on Images for Strap-down Inertial Guidance 会议论文 Zhangjiajie, China, April 24-26, 2020 作者:  Xu Z(徐峥);  Luo HB(罗海波);  Hui B(惠斌);  Chang Z(常铮) 收藏  |  浏览/下载：2/0  |  提交时间：2020/08/01 Autopilot and guidance law design considering impact angle and time 期刊论文 IET CONTROL THEORY AND APPLICATIONS, 2018, 卷号: 12, 期号: 2, 页码: 221-232 作者:  Wang, Xianghua;  Tan, Chee Pin;  Zhou, Donghua 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/11 missile control  impact (mechanical)  autopilot  guidance law design  impact angle  impact time  missile flight  missile LOS angle  missile  line-of-sight angle   Line-of-Sight Rate Estimation Based on UKF for Strapdown Seeker 期刊论文 Mathematical Problems in Engineering, 2015, 页码: 14 作者:  Sun, T. T.;  H. R. Chu;  B. Q. Zhang;  H. G. Jia;  L. H. Guo 收藏  |  浏览/下载：15/0  |  提交时间：2016/07/15 Line-of-sight angular rate estimation of strapdown optical image seeker 期刊论文 Guangxue Xuebao/Acta Optica Sinica, 2014, 卷号: 34, 期号: 6 Sun T.; Chu H.; Jia H.; Zhang Y.; Guo L. 收藏  |  浏览/下载：11/0  |  提交时间：2015/04/24 LOS rate reconstruction and application of roll-pitch seeker (EI CONFERENCE) 会议论文 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China Yang C.; Zhang N.; Jia H. 收藏  |  浏览/下载：17/0  |  提交时间：2013/03/25 Frame motion form of roll-pitch seeker is introduced in this paper. There is corresponding relationship between the frame angle of the roll-pitch seeker and the traditional yaw-pitch seeker. The discrepancy of line-of-sight (LOS) rate of the two seekers is caused by the different frame motion forms. LOS rate reconstruction method of roll-pitch seeker is deduced. Compared to the pure proportional navigation guidance law  the true proportional navigation guidance law is more suitable for the roll-pitch seeker missile guidance. 2011 IEEE.