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浏览/检索结果: 共4条，第1-4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 A Sliding Mode Control Strategy for an ElectroHydrostatic Actuator with Damping Variable Sliding Surface 期刊论文 actuators, 2020, 卷号: 10, 期号: 3 作者:  Mingkang Wang;  Yan Wan;  Rongrong Yang 收藏  |  浏览/下载：3/0  |  提交时间：2020/12/30 sliding mode control  damping variable  electro-hydrostatic actuator  overshoot suppression   Piecewise Linear Weighted Iterative Algorithm for Beam Alignment in Scanning Beam Interference Lithography 期刊论文 Photonic Sensors, 2019, 卷号: 9, 期号: 4, 页码: 344-355 作者:  Y.Song;  Bayanheshig;  S.Li;  S.Jiang;  W.Wang 收藏  |  浏览/下载：0/0  |  提交时间：2020/08/24 Piecewise linear weighted iterative algorithm,beam alignment,scanning,beam interference lithography (SBIL),overshoot suppression,convergence,speed,femtosecond laser,fabrication,gratings,crystal,system,Instruments & Instrumentation,Optics   The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE) 会议论文 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China Zhen D.; Yue Z. 收藏  |  浏览/下载：19/0  |  提交时间：2013/03/25 Autopilot is an important part of aircraft  Under the action of the disturbance torque  for the flight parameters of aircraft Changing in a wide range  the range was about 16km  on the basic of analyzing the typical trajectory  the max height was about 5100m  the trajectory of feature points were selected  the deviation of lateral was about 12m  taking pitch control loop for example  the maximum angle of attack was about 3.6  a sub- PID autopilot was designed using classical control theory  the maximum elevator deflection was less than 5  using single-mode Transient suppression method  the maximum aileron deflection was less than 2  the overload due to control surface transition deflection was avoided when control parameters changing  the maximum roll was less than 5  the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30  the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.  the bandwidth was more than 14rad / s  the settling time was less than 0.7s  the maximum overshoot was 23.3%   A Fuzzy-PID Depth Control Method with Overshoot Suppression for Underwater Vehicle 会议论文 LIFE SYSTEM MODELING AND INTELLIGENT COMPUTING, PT II, 2010-09-17 作者:  Tang, Zhijie[1];  Luojun[2];  He, Qingbo[3] 收藏  |  浏览/下载：1/0  |  提交时间：2019/04/30 Fuzz y-PID  Overshoot Suppression  Depth control  underwater vehicle