One Error Demarcated Method and Experiment of Strap-down Navigation Attitude

被引:0
|
作者
Lin Xueyuan [1 ]
Liu Lingshun [1 ]
Zhou Min [1 ]
机构
[1] Naval Aeronaut & Astronaut Univ, Dept Elect Informat Engn, Yantai 264001, Peoples R China
关键词
strap-down navigation attitude; magnetic sensor; error demarcated method; magnetic deviation;
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
The operation of magnetic course sensor which works as one airborne equipment is tightly related with the effect of carrier environment, because there is larger error in the measured magnetic course angle. The magnetic course sensor can not be used directly in navigation and position. Therefore, this sensor must be compensated to improve the measured accuracy of magnetic course angle when it is used in navigation. The magnetic resistance box and needle is one import magnetic course sensor, of which the magnetic deviation is main error. In the basis of magnetic deviation equation is introduced, the error demarcated method based on LS is mainly deduced by the way of seven parameters and eight positions. The experiment result of this compensated algorithm based on the proposed method proves that the error of magnetic course maintains within 0.5 degrees, thus this proposed method can meet the need of accuracy.
引用
收藏
页码:1575 / 1578
页数:4
相关论文
共 50 条
  • [1] Dynamic Separation Method of Strap-down Inertial Navigation Instrument Error
    Li, Gang
    Xian, Yong
    Wang, Minghai
    [J]. 2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5, 2010, : 4302 - 4305
  • [2] Precision of the attitude algorithm of the strap-down inertial navigation system
    Zhang Wei
    Shi Kui
    Ai Yun
    Guo Juan
    [J]. 9TH INTERNATIONAL SYMPOSIUM ON ADVANCED OPTICAL MANUFACTURING AND TESTING TECHNOLOGIES (AOMATT 2018): OPTICAL TEST, MEASUREMENT TECHNOLOGY, AND EQUIPMENT, 2019, 10839
  • [3] Research on Instrumental Error Compensation of Strap-down Inertial Navigation System
    Jia, Jichao
    Li, Suilao
    Zhao, Changshan
    Long, Rui
    [J]. 2009 INTERNATIONAL ASIA CONFERENCE ON INFORMATICS IN CONTROL, AUTOMATION, AND ROBOTICS, PROCEEDINGS, 2009, : 131 - 133
  • [4] Analysis of error for a rotating strap-down inertial navigation system with fibro gyro
    Ben Y.
    Chai Y.
    Gao W.
    Sun F.
    [J]. Journal of Marine Science and Application, 2010, 9 (4) : 419 - 424
  • [5] Attitude Calculating for a New Strap-down Inertial Navigation System Based on Angular Accelerometers
    Wang, Meiling
    Zheng, Xin
    Liu, Tong
    Wang, Tonglei
    [J]. 2016 IEEE INTERNATIONAL CONFERENCE ON INFORMATION AND AUTOMATION (ICIA), 2016, : 1467 - 1472
  • [6] Vibration Error Compensation for Mobile Vehicle using Strap-down Inertial Navigation System
    Yang, Hai
    Zhang, Rui
    Hoeflinger, Fabian
    Li, Wei
    Reindl, Leonhard M.
    [J]. 2016 13TH INTERNATIONAL MULTI-CONFERENCE ON SYSTEMS, SIGNALS & DEVICES (SSD), 2016, : 401 - 405
  • [7] A Fast Intelligent Algorithm-Based Positioning Error Suppression Method for Strap-Down Inertial Navigation System
    Hongyang, He
    Bao, Li
    Feng, Zha
    Hongqiong, Tang
    [J]. IEEE SENSORS JOURNAL, 2023, 23 (05) : 5278 - 5287
  • [8] A tiny integrated strap-down inertial navigation system
    Pei Hailong
    Zhang Qian
    Luo Pei
    [J]. Proceedings of the 24th Chinese Control Conference, Vols 1 and 2, 2005, : 1263 - 1266
  • [9] Matlab/Simulink software implementation and interfacing of a strap-down inertial attitude method
    Grigorie, T. L.
    Obreja, R.
    Corcau, J.
    Dinca, L.
    [J]. 38TH ANNUAL CONFERENCE ON IEEE INDUSTRIAL ELECTRONICS SOCIETY (IECON 2012), 2012, : 5457 - 5462
  • [10] Numerical Study of an Error Model for a Strap-down INS
    Grigorie, T. L.
    Sandu, D. G.
    Corcau, C. L.
    [J]. APPLICATION OF MATHEMATICS IN TECHNICAL AND NATURAL SCIENCES (AMITANS'16), 2016, 1773