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受油机运动模拟系统设计与建模仿真分析 被引量:3

Design and Modeling Simulation Analysis of Motion Simulation System of Refueled Aircraft
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摘要 提出了一种硬式空中加油地面模拟系统设计方案,并着重介绍了受油机运动模拟系统部分的机械结构及性能指标参数,针对该受油机运动模拟系统各组成部分分别建立动力学模型,通过MATLAB/Simulink仿真工具,建立系统整体仿真模型,通过分析在中度紊流的情况下,受油机运动模拟系统的轨迹,以及受油机在空中的轨迹与受油机运动模拟系统的跟踪轨迹的误差,确定所设计受油机运动模拟系统能够较好地再现受油机在空中的轨迹,满足系统设计要求。 A design scheme of hard type air refueling ground simulation system is presented. It was focused on introduction of the mechanical structure and performance index parameters of the motion simulation system section of refueled aircraft. The dynamic model was established separately for each component of the oil machine movement simulation system. By MATLAB/Simulink simulation tools, the overall system simulation model was established. By analyzing the movement trajectory of the motion simulation system of refueled aircraft and the error between the movement trajectory of the motion simulation system of refueled aircraft and the movement trajectory of the aircraft in the air in the case of moderate turbulence, it is made sure that the desiged motion simulation system of refueled aircraft can better replay the movement trajectory of the aircraft in the air, and meets the system design requirements.
作者 陈娟 赵君伟 付永领 常亮 杨帅 CHEN Juan ZHAO Junwei FU Yongling CHANG Liang YANG Shuai(School of Mechanical Engineering & Automation, Beihang University, Beijing 100191, China School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China)
出处 《机床与液压》 北大核心 2017年第15期10-14,共5页 Machine Tool & Hydraulics
关键词 受油机 运动模拟系统 建模 仿真 Refueled aircraft Motion simulation system Modeling Simulation
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  • 1侯玉燕.国外空中加油技术的发展和展望[J].飞行力学,1994,12(4):14-22. 被引量:20
  • 2隋成城,由勇,杨永田,由俊生.新型歼击机空中加油飞行仿真建模研究[J].系统仿真学报,2005,17(6):1336-1338. 被引量:12
  • 3周建华.飞机尾流涡的危害与研究现状[J].民航经济与技术,1995(11):21-22. 被引量:2
  • 4朱代武.飞机尾流涡旋的速度模型分析[J].中国民航飞行学院学报,2005,16(6):17-20. 被引量:7
  • 5夏小华 高为炳.非线性系统控制及解耦[M].北京:科学出版社,1997..
  • 6Fravolini M L, Ficola A, Napolitano M R, Campa G, Perhinschi M G. Development of Modeling and Control Tools for Aerial Refueling for UAVs [C]//AIAA Guidance, Navigation, and Control Corfferenee and Exhibit, Austin, TX, August 11-14, 2003.
  • 7Joseph P Nalepka, Jacob L Hinchman, Automated Aerial Refueling Extending the Effectiveness of UAVs [C]//AIAA paper 2005-6005.
  • 8Stepanyan Vahram, Lavretsky Eugene, Hovakimyan Naira. Aerial Refueling Autopilot Design Methodology Application to F-16 Aircraft Model [C]//AIAA Guidance, Navigation, and Control Conference and Exhibit 16-19 August 2004, Providence, Rhode Island AIAA 2004-5321.
  • 9Atilla Dogan, Shinya Sato. Flight Control and Simulation for Aorial Refueling [C]//MAA Guidance, Navigation, and Control Conference and Exhibit 15-18 August 2005, San Francisco, California AIAA 2005-6264.
  • 10Pachter M, Houpis C, Trosen D. Design of an Air-to-Air Automatic Refueling Flight Control System using Quantitative Feedback Theory [J]. Intl. Journal of Robust Nonlinear Control, 1997, 37(3): 561-80.

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