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长春光学精密机械与物... [3]
清华大学 [2]
自动化研究所 [2]
北京航空航天大学 [1]
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会议论文 [6]
学位论文 [1]
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Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2016, 卷号: 230, 期号: 6, 页码: 498-511
作者:
Chang, Yafei
;
Yuan, Ruyi
;
Tan, Xiangmin
;
Yi, Jianqiang
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浏览/下载:12/0
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提交时间:2016/09/30
Dual-control Missile
Adaptive Sliding Mode Control
Robustness
Chattering Attenuation
红外多目标实时跟踪方法的研究
学位论文
博士: 中国科学院大学, 2014
穆治亚
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浏览/下载:70/0
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提交时间:2014/08/21
A blended autopilot for dual control missile using generalized predictive and adaptive terminal sliding mode control
会议论文
The 19th World Congress of the International Federation of Automatic Control, Cape Town, South Africa, August 2014
作者:
Chang, Yafei
;
Yuan, Ruyi
;
Fan, Guoliang
;
Yi, Jianqiang
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  |  
浏览/下载:16/0
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提交时间:2016/04/05
Research on the New Missile Actuation System with Dual Independent Closed-Loop
会议论文
International Conference on Design, Manufacturing and Mechatronics (ICDMM), Changsha, PEOPLES R CHINA, 2014-01-01
作者:
Chen, Hui
;
Fu, Yong-Ling
;
Chen, Juan
;
Liu, He-Song
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浏览/下载:2/0
  |  
提交时间:2020/01/06
Missile
Electro-Hydraulic Actuator
Pressure control
A strong coupled CFD-CSD method on computational aeroelastity (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
Xi R.
;
Jia H.
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浏览/下载:62/0
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提交时间:2013/03/25
In this paper
a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime
but not accurate enough in the supersonic regime. 2011 IEEE.
导弹舵机系统非线性参数识别
会议论文
第九届全国振动理论及应用学术会议论文集, 第九届全国振动理论及应用学术会议暨中国振动工程学会成立20周年庆祝大会, 中国浙江杭州, CNKI, 中国力学学会、中国振动工程学会、中国航空学会、中国机械工程学会、中国宇航学会
陆秋海
;
曹学奇
;
戴诗亮
;
LU Qiuhai
;
Cao Xueqi
;
Dai Shiliang
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浏览/下载:8/0
导弹舵机系统非线性参数识别
会议论文
第九届全国振动理论及应用学术会议论文摘要集, Proceedings of the 9th National Conference on Vibration Theory and Application, 第九届全国振动理论及应用学术会议, The 9th National Conference on Vibration Theory and Application, 中国浙江杭州, CNKI, 中国力学学会、中国振动工程学会、中国航空学会、中国机械工程学会、中国宇航学会
陆秋海
;
曹学奇
;
戴诗亮
;
LU Qiu-hai
;
CAO Xue-qi
;
DAI Shi-liang
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浏览/下载:5/0
Research of automatic test technology of parameters used in a dual-CCD TV measure-system (EI CONFERENCE)
会议论文
2nd International Symposium on Advanced Optical Manufacturing and Testing Technologies: Optical Test and Measurement Technology and Equipment, November 2, 2005 - November 5, 2005, Zian, China
Zhao J.
;
Wang L.
;
Li Y.
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浏览/下载:11/0
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提交时间:2013/03/25
This paper describes a kind of automatic test technology of the parameters used in a dual-CCD TV measure-system (TV -MS) .The TV -MS is the ground control equipment of the anti-tank missile and integrates the technologies of optical
machine and electronics. It is important and key component. The main technical parameters of the TV -MS are field of view
zero point
precision
sensitivity
anti-jamming ability
zooming time and focus time
etc. To insure the TV -MS satisfying the tactical and technical requirements and discover fault and reason
a fast and accurate equipment satisfying the test technical parameters of the TV -MS is urgently needed in manufacture and service. Firstly
the parameter test system converted optical signal to electronic signal
implemented automatic control of the invariant illumination of parallel pipeline output. Secondly
data and command delivering
displaying or printing are realized by using 80C196KB. The experiment result shows that the approach of automatic testing of the Parameters used in a dual-CCD TV -MS is successful and it can be used for all tests of the functions and parameters of the TV -MS. The main innovations are to realize the fast
veracious measure of technical parameters of the dual-CCD TV-MS
and integrate the technologies of optics
machineries and electronics. An advanced means is provided to judge the technical states
find malfunctions and discover the reasons in producing and maintaining process. The equipment suited for anti-tank missile systems is given.
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