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航空遥感惯性稳定平台速率环光纤陀螺仪误差建模与补偿 被引量：4

Rate Loop Fiber Optic Gyroscope Error Modeling and Compensation of Inertial Stabilized Platform for Airborne Remote Sensing
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摘要 针对光纤陀螺仪特点,建立了其输出信号的时间序列模型,设计了基于时间序列模型的简化Saga-Husa自适应卡尔曼滤波器,并对光纤陀螺仪的输出信号进行处理。用Allan方差对数据分析结果表明,光纤陀螺仪误差得到有效抑制,并提高了平台的稳定性能。 针对光纤陀螺仪特点,建立了其输出信号的时间序列模型,设计了基于时间序列模型的简化Saga-Husa自适应卡尔曼滤波器,并对光纤陀螺仪的输出信号进行处理。用Allan方差对数据分析结果表明,光纤陀螺仪误差得到有效抑制,并提高了平台的稳定性能。
作者 杜超超 张延顺 李亚军 房建成
机构地区 北京航空航天大学仪器科学与光电工程学院 北京航空精密机械研究所
出处 《航空精密制造技术》 2012年第5期15-19,共5页 Aviation Precision Manufacturing Technology
基金 国家"973"计划项目(2009CB724002) 国家"863"计划(2006AA06Z223)
关键词 惯性稳定平台 航空遥感 时间序列分析 自适应卡尔曼滤波 光纤陀螺仪 inertial stabilized platform airborne remote sensing platform time series analysis adaptive Kalman filter fiber optic gyroscope
分类号 V26 [航空宇航科学与技术—航空宇航制造工程]
  • 相关文献

参考文献8

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二级参考文献22

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共引文献40

同被引文献37

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引证文献4

二级引证文献22

航空精密制造技术
2012年 第5期

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