Analysis of Gyro's Slope Drift Affecting Inertial Navigation System Error

被引:0
|
作者
Gao, Wei [1 ]
Cao, Bing [1 ]
Ben, Yueyang [1 ]
Xu, Bo [1 ]
机构
[1] Harbin Engn Univ, Coll Automat, Harbin 150001, Heilongjiang Pr, Peoples R China
关键词
gyro constant drift; INS; gyro's slope drift; mathematical model;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In the error study of inertial navigation system (INS), the research on error analysis which is caused by gyro drift is limited to the constant drift in the past. Anyway, reality gyro drift is not a long-term unchanging one but varies continuously with time. With the study of systematic errors in depth, we can see that there exists a slope drift in a particular fiber optic gyroscope drift simulation, which may cause serious heading and position errors in the Inertial Navigation System (INS), therefore the research closer to the real situation of the system error model is particularly important. This article, based on mathematical model of gyro constant drift affecting system error, establishes slope drift's mathematical model, and analyses systematic errors caused by gyro drift under the static base by the simulation, and explains the simulation results according to the error model. It makes the research of error analysis in INS more comprehensive, and lays a foundation of further study on dynamic error.
引用
收藏
页码:3757 / 3762
页数:6
相关论文
共 50 条
  • [41] DOPPLER RADAR ERROR EQUATIONS FOR DAMPED INERTIAL NAVIGATION SYSTEM-ANALYSIS
    KASPER, JF
    NASH, RA
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1975, 11 (04) : 600 - 607
  • [42] Observability and alignment error analysis for rapid transfer alignment of inertial navigation system
    Coll. of Automation, Harbin Engineering Univ., Harbin 150001, China
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2007, 29 (12): : 2111 - 2116
  • [43] UNIFIED APPROACH TO INERTIAL NAVIGATION SYSTEM ERROR MODELING
    GOSHENMESKIN, D
    BARITZHACK, IY
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 648 - 653
  • [44] Research on the Dynamic Error of Strapdown Inertial Navigation System
    Yanling Hao
    Jing Gong
    Wei Gao
    Liang Li
    2008 INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION: (ICMA), VOLS 1 AND 2, 2008, : 813 - 818
  • [45] An Improved Method of Geomagnetic Aided Inertial Navigation Algorithm with Gyro and Accelerometer Error Corrected Online
    Song ZhongGuo
    Gao Jiuxiang
    Zhang Jinsheng
    Xi Xiaoli
    2018 ASIA CONFERENCE ON MECHANICAL ENGINEERING AND AEROSPACE ENGINEERING (MEAE 2018), 2018, 198
  • [46] On the development of an inertial navigation error-budget system
    Abdel-Hafez, Mamoun F.
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2011, 348 (01): : 24 - 44
  • [47] Transfer Alignment Design Using a Gyro-free Inertial Navigation System
    Son, Jae Hoon
    Oh, Sang Heon
    Hwang, Dong-Hwan
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2023, 21 (10) : 3348 - 3356
  • [48] Coning algorithm of laser gyro strapdown inertial navigation system in vibrating condition
    Zhong, Mingfei
    Tang, Jianxun
    Jiang, Qiyuan
    Han, Songlai
    Rao, Guyin
    Yuan, Baolun
    Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering, 2014, 43 (08): : 2626 - 2630
  • [49] Microelectromechnical Systems Inertial Measurement Unit Error Modelling and Error Analysis for Low-cost Strapdown Inertial Navigation System
    Ramalingam, R.
    Anitha, G.
    Shanmugam, J.
    DEFENCE SCIENCE JOURNAL, 2009, 59 (06) : 650 - 658
  • [50] Transfer Alignment Design Using a Gyro-free Inertial Navigation System
    Jae Hoon Son
    Sang Heon Oh
    Dong-Hwan Hwang
    International Journal of Control, Automation and Systems, 2023, 21 : 3348 - 3356