机构

• 地质与地球物理研究所 [1]
• 长春光学精密机械与物... [1]
• 西安光学精密机械研究... [1]

采集方式

• OAI收割 [3]

内容类型

• 期刊论文 [2]
• 会议论文 [1]

发表日期

• 2021 [1]
• 2017 [1]
• 2010 [1]

学科主题

• automation... [1]
• engineerin... [1]
• instrument... [1]

筛选

浏览/检索结果: 共3条，第1-3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 3D modeling of multi-radiation source semi-airborne transient electromagnetic response 期刊论文  OAI收割 CHINESE JOURNAL OF GEOPHYSICS-CHINESE EDITION, 2021, 卷号: 64, 期号: 2, 页码: 716-723 作者:  Li Xiu;  Hu WeiMing;  Xue GuoQiang   |  收藏  |  浏览/下载：36/0  |  提交时间：2021/10/09 Semi-airborne transient electromagnetic method  Multi-radiation source  Flight altitude  3D response  Modeling   Multiple Auxiliaries Assisted Airborne Power Line Detection 期刊论文  OAI收割 ieee transactions on industrial electronics, 2017, 卷号: 64, 期号: 6, 页码: 4810-4819 作者:  Shan, Haotian;  Zhang, Jun;  Cao, Xianbin;  Li, Xuelong;  Wu, Dapeng 收藏  |  浏览/下载：49/0  |  提交时间：2017/06/06 Automatic auxiliaries selection  Bayesian network  context  low altitude flight  power line detection   Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文  OAI收割 2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China Chen C.-Q.; Ji Y. 收藏  |  浏览/下载：28/0  |  提交时间：2013/03/25 Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters  a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly  the various sub-systems which affecting flight parameters are analyzed  some mathematical models of the flight parameter simulation platform is established. Secondly  the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity  using C MEX S-function for the complex kinetic equations. Finally  when the models have been established  encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft  the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform  and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft  it shows that the relative deviation of range is 0.47%  the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard  it is demonstrated the platform is reliable  meets the engineering accuracy requirements. 2010 IEEE.