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计算技术研究所 [3]
长春光学精密机械与物... [3]
地理科学与资源研究所 [2]
中国科学院大学 [2]
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力学研究所 [1]
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期刊论文 [11]
会议论文 [6]
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2020 [1]
2019 [2]
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Verification and validation of large eddy simulations of turbulent cavitating flow around two marine propellers with emphasis on the skew angle effects
期刊论文
OAI收割
APPLIED OCEAN RESEARCH, 2020, 卷号: 101, 页码: 15
作者:
Long Y
;
Han CZ
;
Ji B
;
Long XP
;
Wang YW(王一伟)
  |  
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2020/10/29
Cavitation
Cavitating flow
Large eddy simulation (LES)
Marine propeller
Verification and validation (V&V)
Quantitative simulation and verification of upgrade law of sustainable development in Beijing-Tianjin-Hebei urban agglomeration
期刊论文
OAI收割
SCIENCE CHINA-EARTH SCIENCES, 2019, 卷号: 62, 期号: 12, 页码: 2031-2049
作者:
Fang, Chuanglin
;
Liang, Longwu
;
Wang, Zhenbo
  |  
收藏
  |  
浏览/下载:60/0
  |  
提交时间:2020/05/19
Sustainable upgrade law of urban agglomeration
Sustainable upgrade strength of urban agglomeration
Quantitative simulation and verification
Beijing-Tianjin-Hebei urban agglomeration
Quantitative simulation and verification of upgrade law of sustainable development in Beijing-Tianjin-Hebei urban agglomeration
期刊论文
OAI收割
SCIENCE CHINA-EARTH SCIENCES, 2019, 卷号: 62, 期号: 12, 页码: 2031-2049
作者:
Fang, Chuanglin
;
Liang, Longwu
;
Wang, Zhenbo
  |  
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2020/05/19
Sustainable upgrade law of urban agglomeration
Sustainable upgrade strength of urban agglomeration
Quantitative simulation and verification
Beijing-Tianjin-Hebei urban agglomeration
DEVELOPMENT AND PERFORMANCE ANALYSIS OF A FULLY FUNCTIONAL RETURN SIGNAL SIMULATOR FOR HY-2B SCATTEROMETER
会议论文
OAI收割
Valencia, SPAIN, JUL 22-27, 2018
作者:
Wang, Caiyun
;
Guo, Wei
;
Yang, Shuangbao
;
Liu, Peng
  |  
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2019/01/31
Scatteromter
return signal simulator
echo simulation
functional verification
石英砂中甲烷水合物渗透率实验与模型验证
期刊论文
OAI收割
天然气工业, 2017, 卷号: 37, 期号: 12, 页码: 53-60
作者:
李刚
;
李超
;
李小森
;
魏纳
  |  
收藏
  |  
浏览/下载:46/0
  |  
提交时间:2018/12/21
多孔介质
石英砂
甲烷水合物
渗透率
饱和度
实验室模拟
数学模型
验证
Porous media
Quartz sand
Methane hydrate
Permeability
Saturation
Experimental simulation
Mathematical model
Verification
Abstraction-Guided Simulation Using Markov Analysis for Functional Verification
期刊论文
OAI收割
IEEE TRANSACTIONS ON COMPUTER-AIDED DESIGN OF INTEGRATED CIRCUITS AND SYSTEMS, 2016, 卷号: 35, 期号: 2, 页码: 285-297
作者:
Wang, Jian
;
Li, Huawei
;
Lv, Tao
;
Wang, Tiancheng
;
Li, Xiaowei
  |  
收藏
  |  
浏览/下载:12/0
  |  
提交时间:2019/12/13
Abstraction-guided simulation
Markov analysis
semi-formal verification
Design and Analysis of Physical Simulation System for Satellite Rotating Panels
会议论文
OAI收割
2016 IEEE International Conference on Robotics and Biomimetics (ROBIO 2016), Qingdao, China, December 3-7, 2016
作者:
Yin M(尹猛)
;
He Y(贺云)
;
Xu ZG(徐志刚)
;
Liu Z(刘哲)
;
Shao XD(邵晓东)
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2016/12/21
Physical Simulation System
Flexible satellite rotating panels
Structure design
Simulation verification
Generation and verification of three-dimensional network of fractured rock masses stochastic discontinuities based on digitalization
期刊论文
OAI收割
ENVIRONMENTAL EARTH SCIENCES, 2015, 卷号: 73, 期号: 11, 页码: 7075-7088
作者:
Guo, Liang
;
Li, Xiaozhao
;
Zhou, Yangyi
;
Zhang, Yangsong
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2018/06/05
Beishan of Gansu province
Fractured rock masses
Discontinuity network
Stochastic simulation
Verification
Digitalization
A servo control system of dynamic target simulation device for aerial camera (EI CONFERENCE)
会议论文
OAI收割
2nd International Conference on Advanced Design and Manufacturing Engineering, ADME 2012, August 16, 2012 - August 18, 2012, Taiyuan, China
作者:
Ji Q.
收藏
  |  
浏览/下载:31/0
  |  
提交时间:2013/03/25
This article introduces a dynamic target simulation device to evaluate dynamic image quality of the aerial camera. The device simulated the positional relationship of the sky and ground in the laboratory when aerial camera flies at high altitude. And it can be used to inspect camera image quality of aerial camera flying at high altitude in laboratory. At a same time
the article focuses on this servo control system of device
building a control model
and giving control strategy. The servo control system was proved stably and reliably after experimental verification. And it provides a strong guarantee for the test of the dynamic image. (2012) Trans Tech Publications
Switzerland.
The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Zhen D.
;
Yue Z.
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2013/03/25
Autopilot is an important part of aircraft
Under the action of the disturbance torque
for the flight parameters of aircraft Changing in a wide range
the range was about 16km
on the basic of analyzing the typical trajectory
the max height was about 5100m
the trajectory of feature points were selected
the deviation of lateral was about 12m
taking pitch control loop for example
the maximum angle of attack was about 3.6
a sub- PID autopilot was designed using classical control theory
the maximum elevator deflection was less than 5
using single-mode Transient suppression method
the maximum aileron deflection was less than 2
the overload due to control surface transition deflection was avoided when control parameters changing
the maximum roll was less than 5
the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30
the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.
the bandwidth was more than 14rad / s
the settling time was less than 0.7s
the maximum overshoot was 23.3%