机构

• 中国科学院大学 [2]
• 地质与地球物理研究所 [1]
• 长春光学精密机械与物... [1]

采集方式

• iSwitch采集 [2]
• OAI收割 [2]

内容类型

• 期刊论文 [3]
• 会议论文 [1]

发表日期

• 2016 [3]
• 2012 [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 Feasibility of central loop TEM method for prospecting multilayer water-filled goaf 期刊论文  OAI收割 APPLIED GEOPHYSICS, 2016, 卷号: 13, 期号: 4, 页码: 587-597 作者:  Shu, Yan;  Gou-Qiang, Xue;  Wei-Zhong, Qiu;  Hai, Li;  Hua-Sen, Zhong   |  收藏  |  浏览/下载：37/0  |  提交时间：2017/11/17 Central Loop Tem Method  Prospecting Multilayer Water-filled Goaf  Conductive Shielding Layer  Numerical And Theoretical Analysis  Length Of Observation Time  Observation Error  Distinguishable Criterion   An analytical approach to estimate curvature effect of coseismic deformations 期刊论文  iSwitch采集 Geophysical journal international, 2016, 卷号: 206, 期号: 2, 页码: 1327-1339 作者:  Dong, Jie;  Sun, Wenke;  Zhou, Xin;  Wang, Rongjiang 收藏  |  浏览/下载：49/0  |  提交时间：2019/05/09 Numerical approximations and analysis  Reference systems  Computational seismology  Theoretical seismology   Accuracy of the water column approximation in numerically simulating propagation of teleseismic pp waves and rayleigh waves 期刊论文  iSwitch采集 Geophysical journal international, 2016, 卷号: 206, 期号: 2, 页码: 1315-1326 作者:  Zhou, Yong;  Ni, Sidao;  Chu, Risheng;  Yao, Huajian 收藏  |  浏览/下载：67/0  |  提交时间：2019/05/09 Numerical approximations and analysis  Body waves  Surface waves and free oscillations  Theoretical seismology  Wave propagation   Reliable attitude stability control of quad-rotor based on fault-tolerant approach (EI CONFERENCE) 会议论文  OAI收割 2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China 作者:  Gao Q. 收藏  |  浏览/下载：39/0  |  提交时间：2013/03/25 The reliability flight property has received much attention within the aircraft control community throughout the last decades. In this paper  the fault-tolerant control technique is introduced into the attitude stability control system of a quadrotor UAV in order to compensate the influence of the actuators fault of the aircraft. This control scheme is composed of two components: a robust fault detection module using the modelbased observation approach and a reconfigurable controller. Besides the designing procedure  the theoretical analysis of robustness and stability of the designed FTC scheme are also contained in this article. And finally  the availability of the proposed scheme is verified through numerical simulation. 2012 IEEE.