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电动负载模拟器广义连接刚度测试系统研究 被引量:2

Research on generalized coupled stiffness test system of electric load simulator
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摘要 为提高电动负载模拟器的动态性能和加载精度,针对广义连接刚度对系统的动态响应、加载精度和稳定性的影响,设计一种广义连接刚度测试系统,在构建系统的硬件结构和软件功能的基础上,结合广义连接刚度的计算方法及影响因素,提出一种通过调整弹性杆刚度确定最佳广义连接刚度的方法,并对多余力矩、机械谐振、动态特性等影响因素及最佳广义连接刚度进行定量分析。实验结果表明:测试系统功能完善,测试结果准确。另外,在系统获得最佳广义连接刚度时,系统加载曲线与指令曲线完全重合,明显消除多余力矩对系统的干扰,为动态测试舵机性能提供先决条件。 A generalized coupled stiffness test system is designed to enhance the dynamicperformance and loading precision of electric load simulator aiming at the influence of generalizedcoupled stiffness on system dynamic response, loading precision and stability. Combined thecomputing method and influence factors of generalized coupled stiffness, a method determiningoptimal generalized coupled stiffness by adjusting the stiffness of elastic rod is proposed on thebasis of constructing hardware structure and software functions of system. Besides, the extraneoustorque, mechanical resonance, dynamic characteristics and other influential factors and the optimalgeneralized coupled stiffness are quantitatively analyzed. Experimental results show that the testsystem is fully functional and test results are accurate. Besides, the system load curve andcommand curve completely overlap when the system obtains an optimal generalized coupled stiffnessand the interference of the extraneous torque on the system is 'eliminated greatly, providingpreconditions for the dynamic test of the servo performances.
出处 《中国测试》 CAS 北大核心 2017年第3期69-73,共5页 China Measurement & Test
基金 国家国际科技合作项目(2014DFR70650) 山西省科技攻关项目(2015031007-1)
关键词 电动负载模拟器 广义连接刚度 多余力矩 弹性杆 electric load simulator generalized coupled stiffness extraneous torque elastic rod
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  • 1张立勋,王安敏,周继成,吴盛林,刘庆和.位置同步补偿提高飞行器负载模拟器频宽的研究[J].哈尔滨工业大学学报,1995,27(3):123-126. 被引量:6
  • 2Yalla SK, Kareem A. Dynamic Load Simulators Actuation Strategies and Applications. Journal of Engineering Mechanics, 2007, 133(8). 855-863
  • 3王明彦 郭犇 王斌.电动负载模拟器的结构与控制[J].电气传动,2002,32:184-187.
  • 4胡寿松.自动控制原理[M].北京:科学出版社,2002..
  • 5Yoonsu Nam,Jinyoung Lee,Sung Kyung Hong.Force control system design for aerodynamic load simulator[A].In:Proceeding of the American Control Conference[C].Chicago:lllinois USA,2000,7:3043~3047
  • 6Li G Q, Zhao K D, Yuan R B. Study on the Effect of Generalized Coupled Stiffness in the Electro - hydraulic Load Simulator [ C ] . Proceedings of the International Conferenceon Mechanical Engineering and Mechanics 2005. Nanjing : Science Press. China, 2005.
  • 7胡寿松.自动控制原理[M].四版.北京:科学出版社,2002.
  • 8JONES J G. Nonlinear aircraft loads in severe atmospheric turbu- lence[J]. Journal of Aircraft, 2009, 46(5) : 1627 - 1633.
  • 9KARPENKO Mark, SEPEHRI Narlman. Hardware-in-the-loop sim- ulator for research on fault tolerant control of electrohydraulic actu- ators in a flight control application [J ]. Mechatronics, 2009, 19 (7) : 1067 -1077.
  • 10E. Paul,Strauss.Adaptive Load-stand Design for Real-time HWIL JSOW Missile Control Section Characterization. Proceeding of SPIE-the International Society Optical Engineering . 1996

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