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Simulated identification on dynamic characteristics of large heavy-load bearing 期刊论文
Journal of Vibroengineering, 2017, 卷号: 19, 期号: 5, 页码: 3230-3242
作者:  Ouyang, Wu*;  Peng, Lin;  Chen, Runlin;  Yuan, Xiaoyang
收藏  |  浏览/下载：2/0  |  提交时间：2019/12/04
Simulated identification on dynamic characteristics of large heavy-load bearing 期刊论文
JOURNAL OF VIBROENGINEERING, 2017, 卷号: 19, 页码: 3230-3242
作者:  Ouyang, Wu;  Peng, Lin;  Chen, Runlin;  Yuan, Xiaoyang
收藏  |  浏览/下载：6/0  |  提交时间：2019/11/26
Simulated identification on dynamic characteristics of large heavy-load bearing 期刊论文
2017, 卷号: 19, 页码: 3230-3242
作者:  Ouyang, Wu;  Peng, Lin;  Chen, Runlin;  Yuan, Xiaoyang
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/20
Deploying process modeling and attitude control of a satellite with a large deployable antenna 期刊论文
2016, 2016
Zhigang Xing; Gangtie Zheng; Zhigang Xing; Gangtie Zheng
收藏  |  浏览/下载：3/0
Application of the metabolic scaling theory and water-energy balance equation to model large-scale patterns of maximum forest canopy height 期刊论文
GLOBAL ECOLOGY AND BIOGEOGRAPHY, 2016
Choi, Sungho; Kempes, Christopher P.; Park, Taejin; Ganguly, Sangram; Wang, Weile; Xu, Liang; Basu, Saikat; Dungan, Jennifer L.; Simard, Marc; Saatchi, Sassan S.; Piao, Shilong; Ni, Xiliang; Shi, Yuli; Cao, Chunxiang; Nemani, Ramakrishna R.; Knyazikhin, Yuri; Myneni, Ranga B.
收藏  |  浏览/下载：4/0  |  提交时间：2017/12/03
Assessing Landscape Ecological Risk in a Mining City: A Case Study in Liaoyuan City, China 期刊论文
SUSTAINABILITY, 2015
Peng, Jian; Zong, Minli; Hu, Yi' Liu, Yanxu; Wu, Jiansheng; na
收藏  |  浏览/下载：5/0  |  提交时间：2017/12/03
高超声速飞行器大包线跟踪控制关键问题研究 学位论文
工学博士, 中国科学院自动化研究所: 中国科学院大学, 2014
作者:  蒲志强
收藏  |  浏览/下载：200/0  |  提交时间：2015/09/02
Capability of the extended state observer for minimum phase plants with unknown orders and uncertain relative degrees (EI CONFERENCE) 会议论文
31st Chinese Control Conference, CCC 2012, July 25, 2012 - July 27, 2012, Hefei, China
Zhao C.; Yang X.; Xiong J.; Lin X.
收藏  |  浏览/下载：11/0  |  提交时间：2013/03/25
Adaptive control at launching using three loop autopilot (EI CONFERENCE) 会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Zhang Y.
收藏  |  浏览/下载：19/0  |  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.  
入口扰动频率对矩形射流影响的大涡模拟 期刊论文
2010, 2010
蒋平; 郭印诚; 张会强; 王希麟; 林文漪; JIANG Ping; GUO Yin-cheng; ZHANG Hui-qiang; WANG Xi-lin; LIN Wen-yi
收藏  |  浏览/下载：4/0

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