机构

• 海洋研究所 [2]
• 长春光学精密机械与物... [1]
• 武汉物理与数学研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 期刊论文 [2]
• CNKI期刊论文 [1]
• 会议论文 [1]

发表日期

• 2018 [2]
• 2011 [1]
• 2003 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Optimal Initial Error Growth in the Prediction of the Kuroshio Large Meander Based on a High-resolution Regional Ocean Model 期刊论文  OAI收割 ADVANCES IN ATMOSPHERIC SCIENCES, 2018, 卷号: 35, 期号: 11, 页码: 1362-1372 作者:  Li, Xia;  Wang, Qiang;  Mu, Mu   |  收藏  |  浏览/下载：30/0  |  提交时间：2019/08/27 Kuroshio large meander  predictability  ROMS  optimal initial error growth   Optimal Initial Error Growth in the Prediction of the Kuroshio Large Meander Based on a High-resolution Regional Ocean Model CNKI期刊论文  OAI收割 2018 作者:  Xia LIU;  Qiang WANG;  Mu MU   |  收藏  |  浏览/下载：4/0  |  提交时间：2024/12/18 Kuroshio large meander  predictability  ROMS  optimal initial error growth   Adaptive control at launching using three loop autopilot (EI CONFERENCE) 会议论文  OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China 作者:  Zhang Y. 收藏  |  浏览/下载：25/0  |  提交时间：2013/03/25 In order to guarantee the precise initial flight trajectory  control the missile disturbance of large disturbance torque  three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop  combined with the instruction of generalized error  autopilot structure was simplified  and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm  the attitude angle generalized error was -4.4. In the time lasted about 15s  late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes  control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.   Convergence to strong nonlinear rarefaction waves for global smooth solutions of p-system with relaxation 期刊论文  OAI收割 DISCRETE AND CONTINUOUS DYNAMICAL SYSTEMS, 2003, 卷号: 9, 期号: 5, 页码: 1243-1262 作者:  Zhao, HJ;  Zhao, YC 收藏  |  浏览/下载：16/0  |  提交时间：2015/12/03 strong nonlinear rarefaction waves  p-system with relaxation  large initial error