Strapdown INS error model for multiposition alignment

被引：56
|
作者：
Chung, D
Lee, JG
Park, CG
Park, HW
机构：
[1] KWANGWOON UNIV,DEPT CONTROL & INSTRUMENTAT ENGN,SEOUL 139701,SOUTH KOREA
[2] KWANGWOON UNIV,INST NEW TECHNOL,SEOUL 139701,SOUTH KOREA
[3] AGCY DEF DEV,TAEJON 300600,SOUTH KOREA
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1996年 / 32卷 / 04期
关键词：
D O I：
10.1109/7.543857
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The relationship between quaternion errors and tilt angles from true navigation frame to analytic platform frame is newly derived for strapdown inertial navigation system (SDINS). Using the relationship it is shown that the quaternion error model for attitude and velocity is equivalent to the conventional perturbation error model. Based upon the equivalency, the quaternion errors during a multiposition alignment are determined and analyzed. Furthermore, it is shown that the heading rotation of 180 deg achieves the minimal quaternion error for 2-position ground alignment.
引用
收藏
页码：1362 / 1366
页数：5
相关论文
共 50 条
  • [31] STRAPDOWN GUIDANCE ERROR ANALYSIS
    MORTENSEN, RE
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1974, AE10 (04) : 451 - 457
  • [32] ALIGNMENT METHODS FOR STRAPDOWN INERTIAL SYSTEMS
    THOMPSON, EH
    FARRELL, JL
    KNIGHT, JW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1966, 3 (09) : 1432 - &
  • [33] Analysis of influence of Master INS acceleration quantization error on rapid transfer alignment
    Kui, Li
    Wei, Wang
    SEVENTH INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION AND CONTROL TECHNOLOGY: OPTOELECTRONIC TECHNOLOGY AND INSTUMENTS, CONTROL THEORY AND AUTOMATION, AND SPACE EXPLORATION, 2008, 7129
  • [34] Uncertainty estimation for multiposition form error metrology
    Estler, WT
    Evans, CJ
    Shao, LZ
    PRECISION ENGINEERING-JOURNAL OF THE AMERICAN SOCIETY FOR PRECISION ENGINEERING, 1997, 21 (2-3): : 72 - 82
  • [35] PERFORMANCE AND ERROR MODEL OF A SINGLE-DEGREE-OF-FREEDOM STRAPDOWN GYROSCOPE
    STIELER, B
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1970, 18 (11): : 421 - &
  • [36] COVARIANCE ANALYSIS OF STRAPDOWN INS CONSIDERING GYROCOMPASS CHARACTERISTICS
    PARK, HW
    LEE, JG
    PARK, CG
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1995, 31 (01) : 320 - 328
  • [37] System reset of strapdown INS for pipeline inspection gauge
    Ben, Yueyang
    Yang, Jiaolong
    Yin, Donghan
    Li, Qian
    OCEAN ENGINEERING, 2014, 88 : 357 - 365
  • [38] Application of the wavelet packet analysis in the RLG strapdown INS
    Chuang, Guo
    Jian, Wang
    Rong, Fan
    2006 IEEE INTERNATIONAL CONFERENCE ON INFORMATION ACQUISITION, VOLS 1 AND 2, CONFERENCE PROCEEDINGS, 2006, : 926 - 930
  • [39] The Quaternion-Based Attitude Error for the Nonlinear Error Model of the INS
    Zhu, Tiangao
    Liu, Yong
    Li, Wenkui
    Li, Kailong
    IEEE SENSORS JOURNAL, 2021, 21 (22) : 25782 - 25795
  • [40] Direct Gravity Estimation and Compensation in Strapdown INS Applications
    Akeila, Ehad
    Salcic, Zoran
    Swain, Akshya
    PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON SENSING TECHNOLOGY, 2008, : 218 - 223
12345