期刊文献+

基于光学自准直技术的导航系统姿态输入输出方法 被引量:1

Input/output method for INS attitude by optical autocollimation
下载PDF
导出
摘要 基于光学陀螺的单轴旋转式捷联惯性通常采用角度传感器来实现方位角的输出,但其测量结果受角度传感器自身精度、回转轴系、橡胶减震器及防冲击减震器的影响较大。为提高姿态传递精度,提出一种基于自准直仪和多面镜的光学传递方案,通过光学方法将输出平面与惯组直接建立关系,从而减少中间环节,消除角度传感器误差对系统方位角输出带来的误差,可有效避免传统测量中各种因素的影响。通过模拟试验该方案三个姿态角的传递精度均可达到5″以内,满足惯性系统的高精度姿态传递需要。 In single-axis rotating INS with optical gyros, an angle sensor is usually used to realize the attitude's output. But the accuracy of this method is significantly influenced by angle sensor, rotary shaft, rubber absorber, and anti-shock absorber. To solve this problem, an attitude transferring scheme by using autocollimators and polygon mirrors is proposed. The relationship between output plane and IMU is directly established by an optical method, thereby reducing the intermediate steps and effectively avoiding the above influencing factors in traditional method. The simulation results show that the transfer accuracies of the three attitudes are all within 5", which satisfies the need of attitude transfer in high precision INS.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2015年第2期275-280,共6页 Journal of Chinese Inertial Technology
基金 国防科技预研重点项目(A0320132002)
关键词 姿态传递 自准直仪 多面镜 折转光管 attitude transfer autocollimator polygon mirror reflex tube
  • 相关文献

参考文献9

  • 1仲岩,王丹丹,王兴全,王东升,李彦征,孙学成.一种高精度捷联惯组方位引出方法[J].中国惯性技术学报,2014,12(6):845-848. 被引量:2
  • 2牛立,赵慧,范凯峰,张宝玉,王东升.战车用惯性定位定向系统的支架误差分析及补偿[J].中国惯性技术学报,2007,15(5):522-525. 被引量:4
  • 3胡佩达,高钟毓,张嵘,韩丰田.基于三轴摇摆台的高精度姿态试验系统[J].中国惯性技术学报,2013,21(2):271-274. 被引量:9
  • 4Zhang L,Wang A G.Vessel surface equipment attitude measurement based on conventional inertial reference system[J].Advanced Materials Research,2012,629:878-883. 被引量:1
  • 5Johnson G,Waid J,Primm M,et al.Ship attitude accuracy trade study for aircraft approach and landing operations[C]//IEEE Position Location and Navigation Symposium.2012:783-790. 被引量:1
  • 6Gu D Q,El-Sheimy N,Hassan T,et al.Coarse alignment for marine SINS using gravity in the inertial frame as a reference[C]//IEEE Position,Location and Navigation Symposium.2008:961-965. 被引量:1
  • 7Yu Q,Jiang G,Fu S,et al.Fold-ray video metrics method for the deformation measurement of pointer visible large structures[J].Applied Optics,2009,48(24):4683-4687. 被引量:1
  • 8Johnson G,Waid J,Primm M,et al.Ship attitude accuracy trade study for aircraft approach and landing operations[C]//IEEE Position,Location and Navigation symposium.2012:783-790. 被引量:1
  • 9Zhang L,Wang A G.Vessel surface equipment attitude measurement based on conventional intertidal reference system[J].Advanced Materials Research,2012,629:878-883. 被引量:1

二级参考文献14

  • 1张涛,徐晓苏.方位捷联惯导平台系统及其误差分析[J].中国惯性技术学报,2006,14(5):5-8. 被引量:2
  • 2杨常松,徐晓苏.基于动调陀螺的单轴平台寻北仪及其误差分析[J].中国惯性技术学报,2005,13(4):25-29. 被引量:12
  • 3Titterton D H,Weston J L.Strapdown inertial navigation technology[M].USA:American Institute of Aeronautics and Astronautics,Inc.,2004:115-126. 被引量:1
  • 4Farrell J,Barth M.The global positioning system and inertial navigation[M].NewYork:McGraw-Hill,1998:1-320. 被引量:1
  • 5Jordon J W.An accurate strapdown direction cosine algorithms[R].Report TND-5384,NASA.Washington DC,USA,2001. 被引量:1
  • 6Levinson E,Horst J,Willcocks M.The next generationmarine inertial navigator is here now[C]//IEEE PositionLocation and Navigation Symposium.1994:121-127. 被引量:1
  • 7Johnson G,Waid J,Primm M,et al.Ship attitudeaccuracy trade study for aircraft approach and landingoperations[C]//IEEE Position Location and NavigationSymposium.2012:783-790. 被引量:1
  • 8Gu Dongqing,El-Sheimy N,Hassan T,et al.Coarsealignment for marine SINS using gravity in the inertialframe as a reference[C]//IEEE Position,Location andNavigation Symposium.2008:961-965. 被引量:1
  • 9Shockley J,Zetterstrom S.50 years of the central inertialand GPS test facility[J].American Institute of Aeronauticsand Astronautics.2009:1-32. 被引量:1
  • 10张炎华,王立端,战兴群,翟传润.惯性导航技术的新进展及发展趋势[J].中国造船,2008,49(B10):134-144. 被引量:62

共引文献11

同被引文献6

引证文献1

二级引证文献2

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