期刊文献+

带桨间磁流变阻尼器的直升机“地面共振”开-关控制研究 被引量:4

On-off Control for Ground Resonance of Helicopter Using Inter-Connected Blade Magnetorheological Dampers
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摘要 防止直升机出现“地面共振”是直升机研制过程中必须解决的动力学问题。磁流变阻尼器作为可控阻尼器具有结构紧凑、功耗小及输出力大等优点。本文建立了带有桨间磁流变阻尼器的直升机“地面共振”空间模型运动方程 ,采用开 -关 ( on-off)控制方法来抑制“地面共振”,并进行了仿真计算和控制结果分析。结果表明 ,采用桨间磁流变阻尼器抑制“地面共振”比粘弹性阻尼器有更好的可控性。 One of the important problems needed to be solved in the helicopter research and development is to avoid 'ground resonance'. The Magnetorheological (MR) dampers are used as kinds of controllable dampers, which are compact, low operating power and a potential for sufficient forces for applications. The dynamic equations for spatial model of ground resonance of the helicopter with inter connected blade MR dampers are deduced. The on off control methodology is used to suppress the ground resonance. Simulations of the system and analysis for control effectiveness are made. Simulational results show that on off control scheme based on MR dampers can suppress ground resonance of helicopters effectively and the control performance by using inter connected blade MR dampers is better than visco elastic dampers.
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2003年第3期283-287,共5页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 直升机 磁流变阻尼器 地面共振 开-关控制 自激振动 helicopters ground resonance MR dampers on off control
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参考文献5

  • 1顾仲权,陈爱华.直升机“地面共振”的输出反馈最优控制[J].南京航空航天大学学报,1999,31(4):404-409. 被引量:3
  • 2Marathe S, Frahan, Gandhi, et al. Helicopter blade response and aeromechanical stability with a magnetorheological fluid based lag damper [J].Journal of Intelligent Material Systems and Structures, 1998,9 (2) : 272- 282.
  • 3Sela N M, Rosen A. Ground resonance of a helicopter with inter-connected blades [J]. Journal of American Helicopter Society, 1991,36(2) :82-85.
  • 4Li Pang, Kamath G M, Wereley N M. Analysis and testing of a linear stroke magnetorheological damper[R]. AIAA 98-2040, 1998, CP8903(4):2841-2856.
  • 5Zhao Yongsheng, Young T Chor, Wereley N M.Semi-active damping of ground resonance in helicopters using magnetorheological dampers [J].Journal of American Helicopter Society,2001,46(2) :212-225.

二级参考文献5

  • 1包劲松.直升机动力学分析中动力入流模型的理论与试验研究:学位论文[M].南京:南京航空航天大学,1995..
  • 2陈爱华.直升机地面共振的主动控制研究:学位论文[M].南京:南京航空航天大学,1998..
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  • 4包劲松,学位论文,1995年
  • 5陈爱华,顾仲权.旋翼-机体耦合动力稳定性的主动控制现状与发展[J].南京航空航天大学学报,1997,29(6):621-626. 被引量:1

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