许永飞,张士峰.一种基于离心机试验辨识惯导平台误差系数的方法[J].装备环境工程,2018,15(1):1-5. XU Yong-fei,ZHANG Shi-feng.A Method for Identifying Error Coefficients of Inertial Navigation Platform in Centrifuge Test[J].Equipment Environmental Engineering,2018,15(1):1-5.
一种基于离心机试验辨识惯导平台误差系数的方法
A Method for Identifying Error Coefficients of Inertial Navigation Platform in Centrifuge Test
投稿时间:2017-10-21  修订日期:2018-01-15
DOI:10.7643/ issn.1672-9242.2018.01.001
中文关键词:  惯导平台  离心机试验  误差系数辨识  傅里叶分析
英文关键词:inertial navigation platform  centrifuge test  identification of error coefficients  Fourier analysis
基金项目:
作者单位
许永飞 国防科技大学 航天科学与工程学院,长沙 410073 
张士峰 国防科技大学 航天科学与工程学院,长沙 410073 
AuthorInstitution
XU Yong-fei College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China 
ZHANG Shi-feng College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China 
摘要点击次数:
全文下载次数:
中文摘要:
      针对离心机试验中惯导平台误差系数辨识问题,提出了一种基于谐波分析辨识误差系数的方法。首先,根据惯性器件误差模型推导了离心机试验下陀螺和加速度计的输出方程,其输出由各阶谐波分量构成。然后通过傅里叶分析得到各项谐波的幅值。最后根据谐波幅值与各项误差系数之间的关系反解得到各项误差系数。仿真结果验证了方法的有效性。
英文摘要:
      In allusion to identification of error coefficients for inertial navigation platform in centrifuge test, a method based on Fourier analysis was proposed. Firstly, output equation of gyro and accelerometer in centrifuge test was derived according to the error model for inertial device. The output was composed of different order harmonics. Then, the amplitude of each order harmonic was obtained by Fourier analysis. Finally, the error coefficients were obtained based on the relationship between harmonic amplitude expressions and error coefficients. The simulation results show that the proposed method is effective.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第11994116位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号