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Article
Article
Research on Orthogonalization Method of Installation Matrix of Landing IMU for Tianwen-1
- FENG Shiwei1, LIN Song1, LI Yong1,2, XU Lijia1, LI Maodeng1,2
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1. Beijing Institute of Control Engineering,Beijing 100190,China;
2. Science and Technology on Space Intelligent Control Laboratory,Beijing 100190, China
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Received |
Revised |
Published |
12 Dec 2021 |
10 Mar 2022 |
26 Apr 2023 |
Issue Date |
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26 Apr 2023 |
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References
[1] 黄翔宇,徐超,胡荣海,等. 火星精确定点着陆多信息融合自主导航与控制方法研究[J]. 深空探测学报(中英文),2019,6(4):348-357
HUANG X Y,XU C,HU R H,et al. Research of autonomous navigation and control scheme based on multi-information fusion for Mars pinpoint landing[J]. Journal of Deep Space Exploration,2019,6(4):348-357
[2] 薛连莉,翟峻仪,葛悦涛. 2020年国外惯性技术发展与回顾[J]. 导航定位与授时,2021,8(3):59-67
XUE L L,ZHAI J Y,GE Y T. Development and review of foreign inertial technology in 2020[J]. Navigation Positioning and Timing,2021,8(3):59-67
[3] 任顺清,陈希军,王常虹. 惯导检测设备的检测及试验技术(第1版)[M]. 北京:科学出版社,2017.
[4] 秦永元. 惯性导航(第三版)[M]. 北京:科学出版社,2020.
[5] 袁保伦,饶谷音,廖丹. 光学陀螺旋转式惯导系统的安装误差效应分析[J]. 系统工程与电子技术,2010,32(11):2407-2411
YUAN B L,RAO G Y,LIAO D. Mounting error analysis for rotating inertial navigation system with optical gyroscopes[J]. Systems Engineering and Electronics,2010,32(11):2407-2411
[6] 严恭敏,翁浚. 捷联惯导算法与组合导航原理[M]. 西安:西北工业大学出版社,2019.
[7] 王坚,梁建,韩厚增. 低成本IMU的多位置旋转现场标定方法[J]. 中国惯性技术学报,2017,25(3):294-298
WANG J,LIANG J,HAN H Z. Method for low-cost IMU in-field calibration through multi-position rotation[J]. Journal of Chinese Inertial Technology,2017,25(3):294-298
[8] 张福斌,周振华. 一种惯性测量单元非正交安装的单轴转位方法[J]. 中国惯性技术学报,2017,25(2):161-165
ZHANG F B,ZHOU Z H. Single-axis rotation modulation for non-orthogonal installation of IMU[J]. Journal of Chinese Inertial Technology,2017,25(2):161-165
[9] 马亚平,魏国,周庆东. 改进的IMU传感器安装误差正交补偿方法[J]. 传感器与微系统,2016,35(9):9-13
MA Y P,WEI G,ZHOU Q D. An improved method of orthogonal compensation for IMU installation error[J]. Transducer and Microsystem Technologies,2016,35(9):9-13
[10] BRITTING K R. 惯性导航系统分析[M]. 王国臣,李倩,高伟,等译. 北京:国防工业出版社,2017.
[11] 冯士伟,李勇,林松,等. 一种深空探测用3S光纤陀螺石英加计惯性测量单元[C]//月球和深空探测国际学术研讨会. 北京:[s. n. ],2019.
FENG S W,LIN Y,LIN S,at al. A 3-slant IMU composition of fiber optic gyroscope and quartz-accelerometer for deep-space detection[C]//International Symposium on Lunar and Deep Space. Beijing,China:[s. n. ],2019.
[12] GAO P,LI K,SONG T,er al. An accelerometers-size-effect self-calibration method for triaxis rotational inertial navigation system[J]. IEEE Transactions on Industrial Electronics,2018,65(2):1655-1664
[13] CHEN J Y,ZHANG D L,HAN G T,et al. A method for lever arm estimation in INS/GPS integration using direct unscented kalman filter[C]//2020 IEEE 6th International Conference on Computer and Communications (ICCC). Chengdu,China:[IEEE],2020.
[14] 王海波,张汉武,张萍萍,等. 基于横向地球坐标的惯性导航方法[J]. 中国惯性技术学报,2016,12(6):716-722
WANG H B,ZHANG H W,ZHANG P P,et al. Inertial navigation algorithm for polar region based on transverse terrestrial coordinate[J]. Journal of Chinese Inertial Technology,2016,12(6):716-722
[15] GAO P,LI K,WANG L,et al. Four-position heading effect calibration algorithm for rotation inertial navigation system based on fiber optic gyro[J]. Optical Engineering,2016,55(7):1051-1058
[16] 魏莉莉,黄军,傅长松,等. 带斜置元件的光纤陀螺捷联惯组标定方法[J]. 中国惯性技术学报,2015,23(1):14-19
WEI L L,HUANG J,FU C S,et a1. Calibration method of FOG strap down IMU with skewed sensor axis[J]. Journal of Chinese Inertial Technology,2015,23(1):14-19
[17] GAO W,ZHANG Y,WANG J G. Research on inertial alignment and self-calibration of rotary strap down inertial navigation systems[J]. Sensors,2015,15:3154-3171
[18] HU J,CHENG X H,ZHU Y X,et al. On-line integrated correction of attitude and heading for singleaxis rotary SINS[J]. Journal of Southeast University(Natural Science Edition),2016,46(3):494-498
[19] HUANG X Y,LI M D,WANG X L,et al. The Tianwen-1 guidance,navigation,and control for Mars entry,descent,and landing[J]. Space:Science and Technology,2021(1):84-96