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浏览/检索结果: 共5条，第1-5条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Optimization of Locations and Fiber Orientations of Piezocomposite Actuators on Flexible Wings for Aeroelastic Control 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32 作者:  Zhou, Wenya;  Wang, Xiaoming;  Qian, Wei;  Wu, Wenhua 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/02 Flexible wings  Aeroelastic control  Piezocomposite actuators  Fiber orientation  Controllability Gramian matrix  Optimization   Feedback tracking control for dynamic morphing of piezocomposite actuated flexible wings 期刊论文 JOURNAL OF SOUND AND VIBRATION, 2018, 卷号: 416, 页码: 17-28 作者:  Wang, Xiaoming;  Zhou, Wenya;  Wu, Zhigang 收藏  |  浏览/下载：8/0  |  提交时间：2019/12/02 Flexible wings  Shape morphing  Piezocomposite actuators  Aeroelasticity  Tracking control  Linear quadratic Gaussian (LQG) controller   Wind tunnel test and gust load alleviation of flexible wing including geometric nonlinearities with servo control 会议论文 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08 作者:  Chao, A.;  Changchuan, X.;  Yang, M.;  Chao, Y. 收藏  |  浏览/下载：6/0  |  提交时间：2019/12/30 Aspect ratio  Atmospheric turbulence  Aviation  Control nonlinearities  Control surfaces  Finite element method  Flexible wings  Linearization  Proportional control systems  State space methods  Structural dynamics  Two term control systems  Wind stress  Geometric non-linearity  Gust load alleviation  Nonlinear finite element method  Proportional integral derivative controllers  State - space models  Trailing-edge control surfaces  Vertical accelerations  Vortex lattice method  Wind tunnels   Gust Load Alleviation for a Regional Aircraft with Actuator Oscillatory Failure Case 会议论文 IEEE International Conference on Control and Automation, ICCA 作者:  Liu, Y.;  Dong, X.;  Li, Q.;  Ren, Z. 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30 Actuators  Aircraft  Aircraft control  Atmospheric turbulence  Control surfaces  Controllers  Failure (mechanical)  Fault tolerance  Flexible wings  Rigid wings  Actuator fault  Development and applications  Fault tolerant controllers  Flexible aircraft  Gust load alleviation  Passenger comfort  Rigid motions  Suboptimal control techniques  Model reference adaptive control   Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012 作者:  Qi DW;  He GW(何国威);  Liu YM 收藏  |  浏览/下载：48/0  |  提交时间：2013/02/26 Aerospace engineering  Deformation  Exhibitions  Flexible wings  Reynolds number  Rigidity  Vortex flow  Aerodynamic forces  Chord-based Reynolds number  Flexural rigidities  Free stream  Free-stream flow  Lattice boltzmann  Leading-edge vortices  Lift coefficient  Lift force  Particle methods  Pitch rate  Power efficiency  Reduced frequency  Three dimensional space  Time-periods  Tip edge  Trailing edges  Trailing vortex