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兰州理工大学 [7]
大连理工大学 [7]
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会议论文 [19]
期刊论文 [9]
学位论文 [2]
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2011 [31]
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天文学 [1]
微波遥感 [1]
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用小口径望远镜测视宁度的研究
学位论文
硕士, 北京: 中国科学院研究生院(云南天文台), 2011
作者:
宋佳阳
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浏览/下载:32/0
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提交时间:2016/04/06
视宁度
像运动
振动测试
小口径望远镜
Correlations of excited states for sd bosons in the presence of random interactions
期刊论文
PHYSICAL REVIEW C, 2011, 卷号: 83, 页码: 5
作者:
Lei, Y.
;
Zhao, Y. M.
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浏览/下载:6/0
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提交时间:2018/05/31
Random vibration analysis on the support of strapdown inertial navigation system (EI CONFERENCE)
会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Hao X.
;
Li M.
;
Jia H.
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浏览/下载:17/0
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提交时间:2013/03/25
Vibration of the support is an important factor to the accuracy of strapdown inertial navigation. To get vibration characteristics of the support
FEM model of the support was created with Ansys
and then response characteristics were analyzed on the support under the separated random loads during carrier flight
including the phases of subsonic and subsonic. To validate the analysis method
wide band random vibration test was done on the points of the support
which are used for mounting inertial instruments. The comparison of the analysis and the test data shows that the relative error of analysis result is not more than 13%. According to the two results the support structure was improved. Finally random vibration analysis was carried out on the improved one. The result shows that the acceleration response was largely reduced than before. This research can be a reference of performance improvement of the strapdown inertial support and navigation system precision. 2011 IEEE.
Structure optimization of strap-down inertial navigation system support (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
Sun H.
;
Jia H.
;
Wang J.
;
Hao X.
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浏览/下载:20/0
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提交时间:2013/03/25
In order to meet the requirement of inertial navigation components and minimizing the system's weight
and topological optimization was conducted. Then
topological optimization and size optimization were conducted under conditions of random vibration and impact. Firstly
according to the dynamic characteristics of missile and requirement of inertial navigation system
the structure of inertial navigation support was designed according to types of missile connection and space arrangement of electronic components
the method of transforming multi-loading cases to multi-loading constraints was used to optimizing the size of the support under conditions of random vibration and impact. Comparing to the original support structures
RMS accelerations in installed points reduced by 25.2% under random vibration
the weight of optimal structures reduced by 28.1%
the structures also met the requirement of inertial navigation system under condition of impact. The support structure shows improvements in both dynamic characteristic and light weight comparing with the original one. 2011 IEEE.
Design of stable image platform on airborne camera (EI CONFERENCE)
会议论文
2011 International Conference on Advanced Design and Manufacturing Engineering, ADME 2011, September 16, 2011 - September 18, 2011, Guangzhou, China
Qian Y.
;
Yang L.
;
Hu F.
;
Hong X.
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浏览/下载:11/0
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提交时间:2013/03/25
Modulation transfer function resulting from random vibration was analyzed. To conclude that the effect of angular displacement was the major factor. Allowable MTF degradation was represented
and 34dB reduction was achieved at frequency of 100HZ. With the help of MSC.ADAMS simulation software
and convert allowable MTF degradation into stable system design parameters
simulated curve proves correct for isolator
which can guide perfect design for stabilization system. Based on the spatial mechanism and translational principle of parallelogram
and the irrotational displacement mechanism was tested by optical method
an irrotational displacement isolator was developed. It can meet the requirements of irrotational displacement and damp. An instance was given
coupled angle is less than 8?
it can satisfy the demand of aerial imaging. (2011) Trans Tech Publications.
Random vibration analysis of the Deployable Structure for Satellite Antenna
会议论文
2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011, Sanya, China, July 29, 2011 - July 31, 2011
作者:
Zou, Qing
;
Wu, Guangliang
;
Hu, Yong
;
Liu, Xiaoguang
;
Wei, Fuyu
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浏览/下载:25/0
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提交时间:2014/12/15
Simulation of vibrations of Ting Kau Bridge due to vehicular loading from measurements
期刊论文
Structural Engineering and Mechanics, 2011, 卷号: 40, 期号: 4, 页码: 471-488
作者:
Au, F.T.K.
;
Lou, P.
;
Li, J.
;
Jiang, R.J.
;
Zhang, J.
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浏览/下载:2/0
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提交时间:2019/12/03
cable-stayed bridge
dynamic response
finite element
numerical simulation
random vibration
vehicular axle load
Verification of a Cable Element for Cable Parametric Vibration of One-Cable-Beam System Subject to Harmonic Excitation and Random Excitation
期刊论文
ADVANCES IN STRUCTURAL ENGINEERING, 2011, 卷号: 14, 页码: 589-595
作者:
Xia, Yong
;
Wu, Qing-xiong
;
Xu, You-lin
;
Fujino, Yozo
;
Zhou, Xiao-qing
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浏览/下载:2/0
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提交时间:2019/11/21
cable beam interaction
random loading
stay cable
cable element
harmonic loading
auto-parametric vibration
应用时间序列模型的自适应控制
学位论文
2011, 2011
林晓艳
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浏览/下载:2/0
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提交时间:2016/02/14
时间序列分析
最小方差控制
预测控制
Time Series Analysis Method
Minimum Variance Control Method
Predict Control
Vibration-Based Damage Identification Method Using Modified Back-Propagation Neural Networks
其他
2011-01-01
Jin, Hai
;
Nan, Fei
;
金海
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浏览/下载:3/0
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提交时间:2015/07/22
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