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检索条件"机构=Science and Technology on Electormechanical Dynamic Control Laboratory"
376 条 记 录,以下是321-330 订阅
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Three-dimensional suboptimal guidance law for fly-over and shoot-down smart ammunition via virtual target
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Journal of Beijing Institute of technology 2014年 第4期23卷 443-451页
作者: 杨喆 吴炎烜 范宁军 王正杰 National Key Laboratory of Science and Technology on Electro-mechanical Dynamic Control School of Mechatronic EngineeringBeijing Institute of Technology
An optimal burst height is required for the fly-over and shoot-down smart ammunition with an EFP warhead at the instant of explosion which brings a special requirement to the miss distance of the terminal guidance law... 详细信息
来源: 评论
Micro-actuator device characteristics study on lead-based antiferroelectric thick films of (Pb, La)(Zr, Ti)O3
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Gongneng Cailiao/Journal of Functional Materials 2015年 第19期46卷 19060-19064页
作者: An, Kun Chen, Donghong He, Jian Chou, Xiujian Xue, Chenyang Zhang, Wendong National Key Laboratory for Electronic Measurement Technology North University of China Taiyuan China School of Computer Science and Control Engineering North University of China Taiyuan China Key Laboratory of Instrumentation Science & Dynamic Measurement of Ministry of Education North University of China Taiyuan China
Taking the metal alkoxide as a precursor, the wafer grade of (Pb, La)(Zr, Ti)O3(PLZT) anti-ferro-electric thick films were fabricated by the sol-gel process on silicon substrate. Based on the strong field induced stra... 详细信息
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Simulation of characteristics of cloud and fog echo for pluse laser fuze
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Guangxue Jingmi Gongcheng/Optics and Precision Engineering 2015年 23卷 1-7页
作者: Wang, Feng-Jie Chen, Hui-Min Science and Technology on Electromechanical Dynamic Control Laboratory Beijing Institute of Technology Beijing100081 China
Pulse laser fuze is susceptible to the interference of natural environment, such as cloud and fog, and easy to produce a false alarm. Therefore, this paper researches the cloud and fog echo characteristics of the puls... 详细信息
来源: 评论
Design and implementation of an FFT phase difference measuring method
Design and implementation of an FFT phase difference measuri...
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2014 International Conference on Sensors Instrument and Information technology, ICSIIT 2014
作者: Zhu, Xiong Wei Chen, Hui Min Science and Technology on Electromechanical Dynamic Control Laboratory Beijing Institute of Technology Beijing 100081 China
The conventional phase difference measuring methods in the phase-shift laser range finder are usually implemented with complex hardware circuits and phase discrimination algorithm. In this paper an FFT phase differenc... 详细信息
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Thermodynamics study of laser detector with high rotation speed
Thermodynamics study of laser detector with high rotation sp...
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作者: Yue, M.H. Chen, H.M. Science and Technology on Electromechanical Dynamic Control Laboratory Beijing Institute of Technology Beijing100081 China
In this paper, thermodynamics properties of a laser detector applied in 105 mm shrapnel with high rotation speed have been explored. In outer trajectory, aerodynamic heating usually generates because of viscosity, and... 详细信息
来源: 评论
Method for fast transform of pulsed laser peak power
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Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of technology 2015年 35卷 58-61页
作者: Gao, Zhi-Lin Chen, Hui-Min Cai, Ke-Rong Science and Technology on Electromechanical Dynamic Control Laboratory Beijing Institute of Technology Beijing100081 China Shanghai Electro-Mechanical Engineering Institute Shanghai201109 China
The variation law of echoed laser power in the process of fuze encounters the target was analyzed, and a method of simulating the rapid change of echoed laser power by changing the supply voltage and the pulse signal&... 详细信息
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Real-time estimation of maneuvering orbit by compensative modeling of "current" acceleration  27
Real-time estimation of maneuvering orbit by compensative mo...
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27th Conference of Spacecraft TT and C technology
作者: Liu, Y. Cao, Jianfeng Liu, Lei Science and Technology on Aerospace Flight Dynamic Laboratory Beijing100094 China Beijing Aerospace Control Center Beijing100094 China
The unknown maneuver is a key restriction for the real-time spacecraft tracking. For the modeling residual by dynamic of orbits, a compensative modeling method is developed according to the idea of "current"... 详细信息
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dynamic characteristics simulation for terminal trajectory of bomb parachute system in blockade and control ammunition
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Binggong Xuebao/Acta Armamentarii 2015年 36卷 289-294页
作者: Chen, Qing-Sen Song, Rong-Chang Guan, Ping Hao, Yuan Cui, Hai-Bin Science and Technology on Electromechanical Dynamic Control Laboratory Beijing Institute of Technology Beijing100081 China The Huaihai Industrial Group Corporation Limited ChangzhiShanxi046000 China
The blockade and control ammunition based on grenade platform is required to decelerate and despin after launching. Because of its relatively high initial velocity and rotating speed, the robustness of the parachute c... 详细信息
来源: 评论
Earth polar motion parameters high accuracy differential prediction  27
Earth polar motion parameters high accuracy differential pre...
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27th Conference of Spacecraft TT and C technology
作者: Chen, Lue Tang, Geshi Hu, Songjie Chen, Ming Li, Yifei Wang, Mei Sun, Jing Shi, Ming Li, Li National Key Laboratory of Science and Technology on Aerospace Flight Dynamic Beijing100094 China Beijing Aerospace Control Center Beijing100094 China
This paper proposes a method of Earth polar motion parameters prediction by dual differential least-squares (LS) and autoregressive (AR) model. Firstly, polar motion parameters are processed by dual differential metho... 详细信息
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Correcting algorithms of the spinning projectile attitude based on the background magnetic field compensation
Correcting algorithms of the spinning projectile attitude ba...
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2nd International Conference on Precision Mechanical Instruments and Measurement technology, ICPMIMT 2014
作者: Qi, Ke Yu Xiang, Chao Bu, Xiong Zhu Shao, Jun Yu Science and Technology on Electromechanical Dynamic Control Laboratory Xi'an China Shanghai Electro-Mechanical Engineering Institute Shanghai China School of Mechanical Engineering Nanjing University of Science and Technology Nanjing China
At present, traditional navigation method could not provide long-time stability attitude information for the high spinning projectile because of drift errors of micro-inertial sensors. Meanwhile, the projectile attitu... 详细信息
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