机构

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

采集方式

• OAI收割 [4]

内容类型

• 会议论文 [2]
• 期刊论文 [2]

发表日期

• 2017 [2]
• 2012 [1]
• 2011 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4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 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：140/0  |  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   Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文  OAI收割 Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987 作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林) 收藏  |  浏览/下载：53/0  |  提交时间：2017/08/22 Aerodynamic force and moment measurement  10° half-angle cone model  JF12  Real-gas effects  Shock tunnel   Aerodynamic design on China new high-speed trains 会议论文  OAI收割 1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011 作者:  Yang GW(杨国伟);  Yang GW(杨国伟) 收藏  |  浏览/下载：35/0  |  提交时间：2013/02/06 Railroad cars  Railroad transportation  Railroad tunnels  Railroads  Wind effects  Aerodynamic designs  Aerodynamic noise  Aerodynamic performance  Cross-wind effects  High speed trains  Pressure waves  Running conditions  Running tests  Running-in  Wind tunnel experiment   A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文  OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏  |  浏览/下载：67/0  |  提交时间：2013/03/25 In this paper  a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime  but not accurate enough in the supersonic regime. 2011 IEEE.