期刊文献+

新型机载一体化电液作动器的系统设计与仿真 被引量:12

System Design and Simulation of a New Aircraft Electro-Hydrostatic Actuator
在线阅读 下载PDF
导出
摘要 设计了一种用于功率电传的新型一体化电动静液压作动器(EHA),分析该EHA的原理和设计特点,进行系统建模,采用MATLAB/Simulink对其进行仿真。分析了结构参数对系统性能的影响,并应用控制算法提高了系统的性能。仿真结果表明所设计的EHA及其控制方法具有良好的动态性能,达到预定的性能指标。 A new aircraft Electro-Hydrostatic Actuator is designed in order to meet the need of development of aircraft actuation systems. It will be integrated for power-by-wire of airplanes. The paper describes the principle of work and features of the EHA, models and simulates it with MATLAB/Simulink, and analyzes the effects of all structural parameters on the performance. The simulation results have reached the design target of dynamic performances and verified the correctness of the EHA design.
出处 《系统仿真学报》 CAS CSCD 2004年第6期1128-1131,共4页 Journal of System Simulation
基金 博士点学科专项科研基金(20020006006)
关键词 功率电传 电动静液压作动器 机载作动系统 建模与仿真 性能分析 PBW electro-hydrostatic actuator aircraft actuation system modeling and simulation performance analysis
  • 相关文献

参考文献8

  • 1Alan Brown. Actuator research complete [J], NASA the Dryden X-Press, Vol.41, Issue 1, January 15, 1999, http://www.dfrc.nasa.gov/ Newsroom/ X-Press/1999/Jan15/actuator.html
  • 2Steven Croke, Jack Herrenschmidt. More Electric Initiative Power-By - Wire Actuation Alternatives [A], Aerospace and Electronics Conference, 1994(NAECON 94), in: Proceedings of the IEEE 1994 National Aerospace & Electronics Conference [C], New York, N
  • 3Robert Navarro. Performance of an Electro-Hydrostatic Actuator on the F-18 Systems Research Aircraft [R], NASA/TM-97-206224, 1997.
  • 4Stephen C Jensen, Gavin D Jenney, Bruce Raymond, et al. Flight Test Experience With an Electro Mechanical Actuator on the F-18 Systems Research Aircraft [R], NASA/H-2425, 2000.
  • 5[美]玛丽恩·内斯特尔著,程池,黄宇彤,等译.食品安全--令人震惊的食品行业真相[M].北京:社会科学文献出版社,2004.
  • 6付永领, 李军, 罗昀,等.机载一体化电动作动器的新发展及其关键技术[A].见: 中国航空学会控制与应用第十届学术年会暨自控分会成立20周年大会论文集[C].北京:中国航空学会自动控制分会, 2002.329~336Fu Yongling, Li Jun, Luo Yun, et al. The recent development and its critical technologies of airborne integrated electrical actuators[A]. In: The Articles Collection of 10th Academic Anniversary and Automatic Control Department 20th Anniversary of Chinese Society of Aeronautics & Astronautics[C]. Beijing: Automatic Control Department of Chinese Society of Aeronautics & Astronautics, 2002.329~336(in Chinese)
  • 7祁晓野,付永领,王占林.功率电传机载作动系统方案分析[J].北京航空航天大学学报,1999,25(4):426-430. 被引量:46
  • 8李军,付永领,王占林,高波.一种新型机载一体化电液作动器的设计与分析[J].北京航空航天大学学报,2003,29(12):1101-1104. 被引量:29

二级参考文献14

  • 1凌和生.国外飞机电液舵机的发展趋势[J].国际航空,1988,(2):55-57.
  • 2徐树森,焦裕松.飞行控制用的三种作动系统[J].航空科学技术,1997(2):15-17. 被引量:6
  • 3王占林,近代液压控制,1997年
  • 4于敦,国际航空,1989年,2期,53页
  • 5凌和生,国际航空,1988年,2期,55页
  • 6Alan Brown.Actuator research complete[J/OL]. http://www.dfrc.nasa.gov/Newsroom/X-Press/1999/Jan15/actuator.html
  • 7Steven Croke, Jack Herrenschmidt.More electric initiative power-by-wire actuation alternatives[A]. In: Proceedings of the IEEE 1994 National Aerospace & Electronics Conference[C].New York: IEEE, 1994.1338~1346
  • 8于敦.飞机电力作动系统发展方向[R].航空信息研究报告, HY95007.北京: 中国航空信息中心,1995Yu Dun.Development orientation of airborne electrical actuation systems[R].Aero Information research Report, HY95007.Beijing: China Aero Information Center, 1995(in Chinese)
  • 9付永领, 李军, 罗昀,等.机载一体化电动作动器的新发展及其关键技术[A].见: 中国航空学会控制与应用第十届学术年会暨自控分会成立20周年大会论文集[C].北京:中国航空学会自动控制分会, 2002.329~336Fu Yongling, Li Jun, Luo Yun, et al. The recent development and its critical technologies of airborne integrated electrical actuators[A]. In: The Articles Collection of 10th Academic Anniversary and Automatic Control Department 20th Anniversary of Chinese Society of Aeronautics & Astronautics[C]. Beijing: Automatic Control Department of Chinese Society of Aeronautics & Astronautics, 2002.329~336(in Chinese)
  • 10Robert Navarro.Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft[R]. NASA/TM-97-206224, 1997

共引文献63

同被引文献93

引证文献12

二级引证文献100

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部