期刊文献+

光纤捷联惯性测量组合热设计及温度控制技术 被引量:3

Research on Temperature Control and Thermal Design of FOG Inertial Measurement Unit
下载PDF
导出
摘要 因光纤惯组的零偏指标主要受工作环境温度梯度变化影响,为降低高精度光纤惯组的零偏漂移,对惯组内部的光纤陀螺及加速度计进行了高精度温度控制,以实现高精度输出。进行了惯组结构的热特性分析及仿真,提出了两级温控加热结合PWM脉宽控制加热片的整体温控方案。用嵌入式数字温控技术实现了惯组内部的9路温度控制。结果表明:惯组在温度-40-50℃范围内,实现了陀螺零偏稳定性优于0.051(°)/h的工程目标。 The measuring accuracy of FOG inertial measurement unit(IMU)would be influenced by the environment temperature change,and this problem could be solved by the method of high precision temperature control.A temperature control scheme was proposed which was based on the concepts of hierarchical control,sectional control and closed-loop control.From this,a nine-channel digital temperature control system with FPGA architecture was designed from several aspects,such as temperature control scheme,temperature control circuit and temperature control arithmetic.The temperature system contained two-level temperature control and PWM temperature control.The experiments showed that the temperature control system enhanced the environment adaptability.Within the temperature from-40℃to 50℃,the output stable was less than 0.051(°)/h.It provided a practical method for shortening the thermal balance of inertial device after IMU start-up and rapid getting to steady working state.
出处 《上海航天》 2016年第B05期122-126,共5页 Aerospace Shanghai
关键词 光纤 惯组 数字温控 热设计 惯性测量单位 陀螺 稳定 火箭 Fiber optic IMC Digital temperature control Thermal design Inertial measurement unit Gyroscope Stability Launch vehicle
  • 相关文献

参考文献5

二级参考文献17

  • 1刘玉光.惯性平台温控系统精度研究[J].中国惯性技术学报,1996,4(1):35-39. 被引量:5
  • 2马小霞,李汉舟,马建辉.陀螺Fuzzy-PID温度控制系统研究[J].中国惯性技术学报,2004,12(5):58-61. 被引量:5
  • 3李大庆,段建民,綦慧,江存胜.高速数据采集处理系统的设计和实现[J].微计算机信息,2006,22(07Z):191-193. 被引量:9
  • 4任卓恒,宋凝芳,崔佳涛.数字式精密温控对FOG IMU性能的影响[J].北京航空航天大学学报,2007,33(6):694-697. 被引量:4
  • 5Barbour N, Schmidt G. Inertial Sensor Technology Trends[J]. IEEE Sensors Journal, 2001, 1(4): 332-339.
  • 6Gaiffe T. From R&D brassboards to navigation grade FOG-based INS: The Experience of Photonetics/Ixsea[C]//Optical Fiber Sensors Conference Technical Digest, 2002, Vol. 1: 1-4.
  • 7Sanders S J, Strandjord L K, Mead D. Fiber optic gyro technology trends: Honeywell perspective[C]//Optical Fiber Sensors Conference Technical Digest, 2002, Vol.1: 5-8.
  • 8Gaiffe T, Faussot N. Fibre optic gyros for space use[R]. France: ESA, EuroFOG; Report No.1242 SR 06 8, 1999.
  • 9Shupe D.M. Thermally induced nonreciprocity in the fiber optical interferometer[J]. Applied Optics, 1980, 19(5): 654-655.
  • 10[2]Shupe D M.Thermally induced nonreciprocity in the Fiber optical interferometer[J].Applied Optics,1980,19(5):54-655

共引文献92

同被引文献18

引证文献3

二级引证文献1

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