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检索条件"机构=Science and Technology on Aircraft Control Laboratory"
1290 条 记 录,以下是121-130 订阅
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Reachability Analysis and Safety Synthesis of a Class of Human-Computer Collaborative Driving Systems  41
Reachability Analysis and Safety Synthesis of a Class of Hum...
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第41届中国控制会议
作者: Yang-Fan Liu Xiu-Mei Zhang Huai-Ning Wu Science and Technology on Aircraft Control Laboratory School of Automation Science and Electrical EngineeringBeihang University Peng Cheng Laboratory
This work investigates the safety problem for a class of human-computer collaborative driving(H-CCD) systems by the approach of reachable set *** H-CCD system under consideration can monitor the human internal state(H... 详细信息
来源: 评论
Investigation into the characteristics of full-bridge spiral pilot stage
Investigation into the characteristics of full-bridge spiral...
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Wu, Shuai Jiao, Zongxia Yu, Juntao Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
A new high reliable hydraulic pilot stage named full-bridge spiral pilot stage (FBSPS) is proposed in this paper. It utilize a spiral groove on a round pilot spool and two stream holes on the pilot piston form a pair ... 详细信息
来源: 评论
Research on the energy loss characteristics and improving measurement of heat pump
Research on the energy loss characteristics and improving me...
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Liu, Chong Cai, Maolin Wang, Jia Guan, Li Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
Through studying of energy loss characteristics of air source heat pump, this paper focused on energy efficiency of current heat pump systems influenced by seasonal temperature and the problem that the energy loss of ... 详细信息
来源: 评论
Compensation control for the supply pressure fluctuation in electro-hydraulic load simulator
Compensation control for the supply pressure fluctuation in ...
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Han, Songshan Jiao, Zongxia Shang, Yaoxing Wang, Chengwen Wu, Shuai Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
The capability of depressing pressure fluctuation is important to achieve high tracking performance of electro-hydraulic load simulator (EHLS). This paper summarizes the major factors that may cause the pressure fluct... 详细信息
来源: 评论
Research on expansion ratio of air power engine system
Research on expansion ratio of air power engine system
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Yu, Qihui Cai, Maolin Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
To increase the energy utilization rate of compressed air, the expansion ration is optimized based on single-staged compressed air power system by building mathematical method with the basic thermodynamic theory. Two-... 详细信息
来源: 评论
Modeling and analysis of pneumatic loading system
Modeling and analysis of pneumatic loading system
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Qiong, Wei Jiao, Zongxia Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
This paper analyses the fluid dynamic, thermodynamics and kinetic characteristics of a pneumatic loading system, and the detailed nonlinear model is derived and simulated. This model is verified by experiment. The inf... 详细信息
来源: 评论
The process of compressed air energy storage(CAES) analysis
The process of compressed air energy storage(CAES) analysis
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2013 International Conference on Materials for Renewable Energy and Environment, ICMREE 2013
作者: Yu, Qihui Cai, Maolin Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
Future sustainable energy systems call for the introduction of integrated storage technologies. One of these technologies is compressed air energy storage (CAES). In this paper, the principle of CAES is introduced, th... 详细信息
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The design of nonlinear flight control system of hypersonic cruise vehicle based on nonlinear disturbance observer
The design of nonlinear flight control system of hypersonic ...
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3rd International Conference on Instrumentation and Measurement, Computer, Communication and control, IMCCC 2013
作者: Lian, Chengbin Bai, Cheng Ren, Zhang Shao, Xingyue Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
Hypersonic vehicle's nonlinear dynamics system is highly nonlinear, multivariable coupled and includes uncertain parameters. To solve this problem, a new back stepping controller is designed based on nonlinear dis... 详细信息
来源: 评论
The application of multipoint rotate-vector optimization method on the On-line Identification based Optimal control (OIOC
The application of multipoint rotate-vector optimization met...
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2011 International Conference on Fluid Power and Mechatronics, FPM 2011
作者: Zhang, Boya Jiao, Zongxia Kang, Rongjie Wu, Shuai Zhao, Pan Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
The basic rotate-vector optimization method (BROM) is a direct optimization algorithm and is valuable to engineering application. Multipoint rotate-vector optimization method (MROM) is an improved algorithm based on B... 详细信息
来源: 评论
Reliability analysis of flight control system for large civil aircraft with imperfect fault coverage model
Reliability analysis of flight control system for large civi...
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2012 3rd Annual IEEE Prognostics and System Health Management Conference, PHM-2012
作者: Xiong, Xiao Zhang, Ping Science and Technology on Aircraft Control Laboratory Beihang University Beijing China
Reliability of flight control system (FCS) is a key factor of the aircraft safety. Therefore, redundant technology and Built-in Test (BIT) technology are usually adapted by flight control system for modern large civil... 详细信息
来源: 评论