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北京航空航天大学 [3]

厦门大学 [1]

数学与系统科学研究院 [1]

自动化研究所 [1]

沈阳自动化研究所 [1]

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	Dynamic numerical investigation of airborne vapor cycle cooling system 会议论文 IET Conference Publications 作者: Miao, Z.; Liping, P. 收藏 \| 浏览/下载：10/0 \| 提交时间：2019/12/30 Computer simulation Cooling systems Electronic equipment Evaporators Flight envelopes Flight simulators Oscillators (electronic) Refrigeration Temperature control Thermoelectric equipment Airborne equipments Dynamic performance Electronic expansion valves Management technologies Numerical investigations Refrigeration capacity Refrigeration cycles Vapor cycles Electronic cooling
	Blade design and aerodynamic performance numerical simulation on ram air turbine [冲压空气涡轮叶片设计和气动性能数值模拟] 期刊论文 Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2018, 卷号: 44, 页码: 1387-1394 作者: Ji, F.; Zhang, M.; Wang, R.; Wang, Y.; Du, F. 收藏 \| 浏览/下载：19/0 \| 提交时间：2019/12/30 Air Compressed air motors Computation theory Computational fluid dynamics Computer simulation Flight envelopes Gas turbines Magnetorheological fluids Numerical models Rats Structural frames Turbomachine blades Wind turbines Aero-dynamic performance Blade design Blade-element theory Computational fluid dynamics methods Dynamic performance Ram air turbines Rotating turbines Rotor power coefficients Turbine components
	On-line aerodynamic identification of quadrotor and its application to tracking control 期刊论文 IET CONTROL THEORY AND APPLICATIONS, 2017, 卷号: 11, 期号: 17, 页码: 3097-3106 作者: Lei, Wenchao; Li, Chanying 收藏 \| 浏览/下载：127/0 \| 提交时间：2018/07/30 helicopters autonomous aerial vehicles mobile robots trajectory control compensation nonlinear control systems discrete time systems aerodynamics online aerodynamic identification quadrotor tracking control aerodynamic effects quadrotor-type unmanned aerial vehicles recursive least squares algorithm aerodynamic parameters accelerometer nonlinear discrete-time trajectory tracking controllers aerodynamic compensation large-acceleration flight regime
	Partition method for improvement of piecewise linear model with full envelope covered 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2016, 卷号: 31, 页码: 3042-3053 作者: Yang, S.-B.; Wang, X.; Long, Y.-F.; Li, Z.-P.; Hu, Z.-Z. 收藏 \| 浏览/下载：6/0 \| 提交时间：2019/12/30 Aerodynamics Flight simulators Mach number Nonlinear systems Partitions (building) Piecewise linear techniques Sea level Turbofan engines Ambient conditions Corrected parameters Full envelope Operating condition Piecewise linear modeling Real time requirement Standard conditions Static conditions Flight envelopes
	高超声速飞行器大包线跟踪控制关键问题研究学位论文工学博士, 中国科学院自动化研究所: 中国科学院大学, 2014 作者: 收藏 \| 浏览/下载：182/0 \| 提交时间：2015/09/02 高超声速飞行器大包线轨迹线性化自抗扰主动抑制 Hypersonic vehicle Large envelope Trajectory linearization control Active disturbance rejection control Active suppression
	Robust stablization for a class of large envelope flight control systems 其他 2011-01-01 Cheng, Lixia; Yan, Yabin; Zeng, Jianping; 曾建平收藏 \| 浏览/下载：3/0 \| 提交时间：2015/07/22 Computer control systems Computer science Control system stability Control systems Convex optimization Education computing Flight envelopes Robust control Stability criteria State feedback
	Active modeling based model predictive control for yaw-heave coupling dynamics of unmanned helicopters in full flight envelope 会议论文 AUVSI Unmanned Systems North America Conference 2009, Washington, DC, United states, August 10-13, 2009 作者: 收藏 \| 浏览/下载：17/0 \| 提交时间：2012/06/06 Actuators Controllers Dynamics Flight envelopes Helicopters Predictive control systems Robust control

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