机构

• 力学研究所 [3]
• 长春光学精密机械与物... [2]
• 地理科学与资源研究所 [1]
• 数学与系统科学研究院 [1]

采集方式

• OAI收割 [7]

内容类型

• 期刊论文 [5]
• 会议论文 [2]

发表日期

• 2023 [1]
• 2019 [2]
• 2017 [1]
• 2014 [1]
• 2012 [1]
• 2011 [1]
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学科主题

筛选

浏览/检索结果: 共7条，第1-7条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Reconstruction of the hourly fine-resolution apparent temperature (Humidex) with the aerodynamic parameters 期刊论文  OAI收割 SCIENCE OF THE TOTAL ENVIRONMENT, 2023, 卷号: 866 作者:  Wu, Xilin;  Ge, Yong;  Gong, Daoyi;  Zhang, Xining;  Hu, Shan   |  收藏  |  浏览/下载：27/0  |  提交时间：2023/04/06 Apparent temperature  Reconstruction model  Numerical simulation data  Fine spatiotemporal resolution  Aerodynamic parameters  Downscaling   Characteristic of a multistage reheating radial inflow in supercritical compressed air energy storage with variable operating parameters 期刊论文  OAI收割 PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2019, 卷号: 233, 期号: 3, 页码: 397-412 作者:  Li H;  Li W;  Zhang XH;  Zhu YLi;  Zuo ZT   |  收藏  |  浏览/下载：126/0  |  提交时间：2019/06/10 Supercritical compressed air energy storage  aerodynamic performance  multistage  variable operating parameters  radial inflow turbine   On-line aerodynamic identification of quadrotor and its application to tracking control 期刊论文  OAI收割 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：139/0  |  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   Influences of aerodynamic loads on hunting stability of high-speed railway vehicles and parameter studies 期刊论文  OAI收割 Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 6, 页码: 889-900 作者:  Zeng XH(曾晓辉);  Wu H(吴晗);  Lai J(赖姜);  Sheng HZ(盛宏至) 收藏  |  浏览/下载：32/0  |  提交时间：2015/02/16 Hunting stability  Linear critical speed  Nonlinear critical speed  Aerodynamic loads  Suspension parameters  Orthogonal experimental design   Trajectory tracking control of a quad-rotor UAV based on command filtered backstepping (EI CONFERENCE) 会议论文  OAI收割 2012 3rd International Conference on Intelligent Control and Information Processing, ICICIP 2012, July 15, 2012 - July 17, 2012, Dalian, China Gong X.; Bai Y.; Peng C.; Zhao C.; Tian Y. 收藏  |  浏览/下载：30/0  |  提交时间：2013/03/25 A quad-rotor unmanned aerial vehicle is an under-actuated  strong coupled nonlinear system with parameters uncertainty and unknown external aerodynamic disturbance. The trajectory tracking control system with a nested double-loops structure is designed in this paper according to the coupling characteristic between the attitude angles and translational position. A PD control algorithm is proposed in the translational outer-loop to export the desired attitude signals to the attitude inner-loop. An adaptive backstepping control algorithm is designed in the inner-loop with respect to the uncertain rotational inertia and un-modeled disturbance  while in order to reduce the computational complexity the command filtered approach is introduced into the designing procedure. And finally  the numerical simulation results are presented for the trajectory tracking stabilization of a Quad-rotor  which demonstrates the excellent performance of the proposed control system and illustrate its robustness in face of disturbance and uncertain parameters. 2012 IEEE.   Study of experimental design and Response Surface method for surrogate model of computational simulation (EI CONFERENCE) 会议论文  OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China Xi R.; Jia H.; Xiao Q. 收藏  |  浏览/下载：21/0  |  提交时间：2013/03/25 While the high-precision simulation is widely used in science and technology  Design of Experiment (DOE) based on Response Surface (RS) method can be employed in surrogate model to reduce the cost and error. In order to illustrate the relationship between parameters and response features  several DOE methods and Response Surface (RS) method are studied. The author used polynomial regression and RBF neural network based on orthogonal array to build a rocket aerodynamic discipline surrogate model respectively which proved their feasibility. From the results of the test case  conclusion is drawn that characteristic as well as acclimatization of DOE methods and different approximation should be considered for different issues  so the factors of cost and accuracy could reach a balance synthetically. 2011 IEEE.