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基于LabVIEW的电控旋翼测控系统设计 被引量:8

Design of Measurement and Control System for Electrically Controlled Rotor Based on LabVIEW
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摘要 以电控旋翼综合试验台为研究对象,基于LabVIEW设计开发了一套电控旋翼测控系统。采用自顶向下的设计方法,将各个需要实现的功能模块化,供顶层统一调用。该测控系统整合了测控系统中各个硬件功能,有效实现了系统运行状态反馈、设备控制、控制参数在线发送、数据实时采集与储存、以及旋翼状态监视系统自动保护等功能。试验实测表明:所开发的电控旋翼测控系统能够实现所需的各项功能并满足性能要求。 A set of electronic control system for the measurement and control of the rotor is developed based on LabVIEW for the integrated test platform of the electrically controlled rotor (ECR). Using the top-down design method, each function is modularized and invoked by the top. Measure and control sys- tem integrates all hardware functions to realize the system state feedback, equipment control, control parameters on-line transmission, data real-time acquisition and storage, as well as automatic protection of rotor condition monitoring system. Experimental results show that the developed system can realize the required functions and meet the performance requirements.
作者 董祥见 陆洋
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2017年第2期251-257,共7页 Journal of Nanjing University of Aeronautics & Astronautics
基金 国家自然科学基金(51375229)资助项目
关键词 LABVIEW 电控旋翼 测控系统 LabVIEW electrically controlled rotor measure and control system
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  • 1陆洋,王浩文,高正.用于电控旋翼气弹分析的带襟翼翼型气动力模型[J].空气动力学学报,2005,23(2):243-247. 被引量:6
  • 2王志新,谷云东,李洪兴.三水箱多变量液位控制实验设计[J].实验技术与管理,2007,24(1):32-36. 被引量:14
  • 3ANDREW KENNEDY. Securing the. NET programming model[ J ]. Theoretical Computer Science,2006,364 (3) : 311-317.
  • 4KARLI WATSON, CHRISTIAN NAGEL. Beginning Visual C# 2005 [ M ].北京:清华大学出版社,2006.
  • 5Leishman J G,Beddoes T S.A generalized model for airfoil unsteady aerodynamic behavior and dynamic stall using the indicial method[A].American Helicopter Society 42nd Annual Forum[C].June,1986:243-265.
  • 6Hariharan N,Leishman J G.Unsteady aerodynamics of a flapped airfoil in subsonic flow by indicial concepts[A].36th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference[C].April,1995:613-634.
  • 7Aiken E,Ormiston R,Young L A.Future directions in rotorcraft technology at ames research center[A].American Helicopter Society 56th Annual Forum[C].2000:10-30.
  • 8陆洋,王浩文.电控伺服襟翼旋翼-一种新概念旋翼系统[A].第十八届全国直升机年会论文集[C].昆明:2002:7-12.
  • 9Shen J W,Chopra I.Actuation requirements for a swashplateless helicoter control system with trailing-edge flaps[R].AIAA-2002-1444.
  • 10Shen J W,Chopra I,Johnson W.Performance of swashplateless ultralight helicopter rotor with trailing-edge for primary flight control[A].American Helicopter Society 59th Annual Forum[C].2003:256-266.

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