摘要
半球谐振陀螺仪受到温度影响产生漂移。针对半球谐振陀螺组合设计了一套基于脉宽调制的温控系统。通过对陀螺组合温控方式的选取、均匀对称性结构设计、热模型建模,利用FPGA对陀螺仪进行温控系统设计。实验表明,温控系统精度为±0.1℃,满足陀螺性能要求。
To decrease the temperature drift of the hemispherical resonant gyroscope,a temperature control system based on pulse width modulation is designed for hemispherical resonator gyro in this paper.Through the selection of temperature control mode for gyro combination,uniform symmetrical structure design and thermal model modeling,the temperature control system of gyroscope is designed using FPGA.The experiment shows that the temperature control system has a precision of ±0.1℃,which meets the performance requirements of the gyro.
引文
[1]Rozelle D M.The hemispherical resonator gyro:From wineglass to the planets[J].Spaceflight Mechanics,2009,134:1-26.
[2]高胜利.半球谐振陀螺的分析与研究[D].哈尔滨:哈尔滨工程大学,2008.
[3]潘瑶,曲天良,杨开勇,等.半球谐振陀螺研究现状与发展趋势[J].导航定位与授时,2017,4(2):9-13.
[4]吕志清.半球谐振陀螺(HRG)信号处理技术[J].中国惯性技术学报,2000,8(3):58-61.
[5]王栋.高精度陀螺温控系统的工程实现研究[D].哈尔滨:哈尔滨工业大学,2006.
[6]倪受东,吴洪涛,朱剑英.微型半球陀螺仪的误差源研究[J].传感器与微系统,2007,26(1):30-32.
[7]李广胜,蒋英杰,孙志强,等.基于多项式模型的半球谐振陀螺温度漂移建模[J].测试技术学报,2009,23(6):496-500.
[8]周小刚,汪立新,佘嫱,等.半球谐振陀螺温度补偿与试验研究[J].宇航学报,2010,31(4):1083-1087.
[9]齐轶楠,赵辉,赵万良,等.半球谐振陀螺组合零偏稳定性提高技术研究[J].导航定位与授时,2015,2(6):63-67.
[10]李艳娟,朱艳芳,胡琪波.抑制超声波电机温度变化的应用设计[J].导航定位与授时,2016,3(1):47-52.