期刊文献+

三轴气浮台自重作用下旋转角速度的研究

The Rotational Angular Velocity Research of Three-Axis Air Bear Testbed Under the Control of Gravity
下载PDF
导出
摘要 三轴气浮台旋转过程中会存在重心与旋转轴不重合的情况,这样就会有外力拒产生,从而影响气浮台的正常运转。因此如何解决气浮台由于重心偏移产生的附加力矩问题则是提高其运转精度的关键,必须确定其重心偏移位置,进而对其进行补偿,获取三轴气浮台在自重作用下其旋转角速度的精确值则是确定重心位置的关键步骤,从解决实际问题出发,通过传统的数学方法计算出的结果与实体建模进行动态仿真输出的速度进行对比,指出前者使用的局限性,以及使用后者的可行性。 When in working situation, three-axis air bear will not work correctly if its center of gravity and rotating shaft are not in the same position because of the exist of gravitational torque. So how to solve the gravitational torque is the main process to improve platform working accuracy. For solving that problem, the barycenter position must be confirmed. And how to get the correctly rotational angular velocity is the main step to determine the location of the barycenter. With the contrast of traditional method and dynamic simulation, which are used to measure rotational angular velocity, the conclusion can be got that dynamic simulation is a more available way to test velocity than traditional method.
出处 《机械设计与制造》 北大核心 2014年第7期81-83,共3页 Machinery Design & Manufacture
基金 辽宁省自然科学基金(201202161)
关键词 三轴气浮台 重心 动态仿真 旋转角速度 Three-Axis Air Bear Testbed Center of Gravity Dynamic Simulation Rotational Angular Velocity
  • 相关文献

参考文献7

二级参考文献37

  • 1吴玉山.地球模拟器的研制概况[J].控制工程(北京),1993(4):14-16. 被引量:1
  • 2李季苏,吴振嵩.测试单轴气浮台转动惯量的一种方法[J].航天控制,1994,12(3):69-72. 被引量:7
  • 3宋晓龙.全轨道实时星模拟器[J].系统仿真学报,1995,7(2):40-45. 被引量:7
  • 4程云鹏.矩阵论[M].西安:西北工业大学出版社,1998..
  • 5周军.某卫星天线指向复合控制全物理仿真试验系统研制报告[R].西安:西北工业大学航天学院,2004..
  • 6J. Prado, G. Bisiacchi. Dynamic Balancing For A Satellite Attitude Control Simulator. Instrumentation And Development Vol. 4 Nr. 5.
  • 7Young J S. Development of an Automatic Balancing System for a Small Satellite Attitude Control Simulator[D]. Masters Thesis. Uath State University, 1998.
  • 8Schwartz J S, Peck M A, Hall C D. Historical review of spacecraft simulators[A]. AAS/AIAA Space Flight Mechanics Meeting[C], Ponce, Puerto Rico, 2003.
  • 9D. Miller, et al. SPHERES: A testbed for long duration satellite formation flying in micro-gravity conditions[A]. Proceedings of the AAS/AIAA Space Flight Mechanics Meeting[C]. Clearwater, Florida, January 23-26, 2000: 167-179.
  • 10Glover K E. Development of a large support surface for an air-bearing type zero-gravity simulator[R], NASA Technical Memorandum NASA-TM-X-72780.

共引文献54

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