期刊文献+

直升机仿真模拟训练软件系统设计实现 被引量:2

Design and Realization of Helicopter Simulation Training Software System
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摘要 针对直升机仿真与地面模拟训练的需求,以VC++和Vega为开发工具,研制了一套具有三维视景显示功能的软件系统。通过编写直升机各执行机构的递推运算程序实现直升机模型的解算,用MFC设计直升机"操纵台"与"驾驶杆"界面,在Vega配置的视景仿真环境中显示直升机飞行姿态,以GDI为辅助工具编写虚拟仪表和曲线显示窗口,实时显示直升机姿态角、航向角和速度等飞行数据,实现了直升机仿真与模拟训练功能。实际运行结果表明,该系统仿真效果逼真,达到了设计要求,具有较好的实用性。 According to the requirements of helicopter simulation and training, a set of software system with three - dimension visual display function was developed based on VC + + and Vega. In order to realize the function of helicopter simulation and training, the solution of the helicopter model is achieved by the recursive operations program of the actuators, the helicopter" console" and " column" interfaces are designed based on MFC,the flight attitude is displayed in the visual simulation environment configured in Vega, the flight data such as attitude angles, heading angle and velocity is displayed in real time through virtual instruments and curve display windows which are designed by GDI as the assistant tool. It is shown that the simulation resuhs are realistic, and the system achieves design specification that is very practical
出处 《微处理机》 2011年第5期46-49,共4页 Microprocessors
关键词 直升机 模拟训练 视景仿真 图形界面 Helicopter Simulation training Visual simulation GDI
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  • 1MultiGen-Paradigm, Inc. Vega Lynx User's Guide. Version 3.7 for Windows NT and Windows 98 [Z]. MultiGen- Paradigm, Inc. December 2000.
  • 2龚桌蓉.可选模块的使用与开发[M].北京:国防工业出版社,2003.
  • 3丁斌,祖家奎.基于虚拟现实的无人机三维可视化仿真[J].计算机测量与控制,2007,15(12):1769-1771. 被引量:16

共引文献4

同被引文献23

  • 1段镖,严峰,赖水清.基于FlightGear的无人直升机飞行控制系统仿真环境建设[J].直升机技术,2010(4):58-63. 被引量:6
  • 2蔡儒冠.运用Authorware7.0制作多媒体课件的几点技巧[J].中国电化教育,2004(8):76-78. 被引量:14
  • 3韶亚军.多媒体创作精灵Autitorware实战技巧大全[M].北京:电脑爱好者杂志社,2002;232-238.
  • 4Yi-Rui Tang, Yangmin Li. Development of a laboratory HILS testbed system for small UAV helicopters [C]// Proceedings of the 6th IASTED International Conference on Biomechanics; Proceedings of the Second IASTED International Conference on Robotics. Pittsburgh, USA: ACTA Press, 2011: 428-436.
  • 5Seongpil Kim, Agus Budiyono. Control system design and testing for a small-scale autonomous helicopter [J].Aircraft Engineering and Aerospace Technology (S0002-2667), 2010, 82(6): 353-359.
  • 6Bryan Godbolt. Experimental Validation of a Helicopter Autopilot Design using Model-Based PID Control [J]. Journal of Intelligent & Robotic Systems (S0921-0296), 2013, 70(1/4): 385-399.
  • 7Johannes Hofmann, Antje Dittmer. Model-based control of the flying helicopter simulator: evaluating and optimizing the feedback controller [J]. CEAS Aeronautical Journal (S 1869-5582), 2011, 2(1/4): 43-56.
  • 8Advanced Rotorcraft Technology, Inc. FLIGHTLAB Theory Manual, Volume I [M]. Charleston, USA: Advanced Rotorcraft Technology, Inc. 2011: 7-180.
  • 9He Chengjian. Finite State Dynamic Wake Interference Modeling for Rotorcraft Simulation [C]// American Helicopter Society 53rd Annual Forum, Virginia Beach, Virginia, USA: AHS, 1997: 973-987.
  • 10GJB5449-2005.直升机飞行模拟器通用要求[S].

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