Strapdown INS initial alignment in inertial frame using H∞ filter

被引:0
|
作者
机构
[1] Pei, Fujun
[2] Liu, Xuan
[3] Zhu, Li
来源
Pei, F. (fujunpei@sina.com) | 1600年 / Binary Information Press卷 / 10期
关键词
Alignment error models - Dynamic disturbances - Inertial frames - Initial alignment - Misalignment angles - Random disturbances - Strap-down inertial navigation systems - Strapdown INS;
D O I
10.12733/jcis9764
中图分类号
学科分类号
摘要
Initial alignment is the key procedure in the strapdown inertial navigation system (INS), which directly relates to the working precision of strapdown INS. But the tradition alignment method can't finish alignment under the dynamic disturbance condition. In this paper, a novel alignment method using H∞ filter was investigated to solve this problem. In the coarse alignment procedure, the invariance property of gravity in the inertial frame was used to deal with the disturbances. In the fine alignment procedure, strapdown INS alignment error model under the dynamic condition was established. Moreover, because of the uncertainty observation noise in the velocity measurements, the H∞ robust filter was designed to estimate the misalignment angles accurately. Finally, simulation results demonstrated that the proposed method can depress the random disturbances more effectively than the traditional alignment method. © 2014 Binary Information Press.
引用
收藏
相关论文
共 50 条
  • [1] Initial Alignment for Strapdown Inertial Navigation System Based on Inertial Frame
    Sun, Feng
    Cao, Tong
    Xu, Bo
    Ben, Yueyang
    Wang, Yudan
    2009 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, VOLS 1-7, CONFERENCE PROCEEDINGS, 2009, : 3751 - 3756
  • [2] In-Flight Alignment Using H∞ Filter for Strapdown INS on Aircraft
    Pei, Fu-Jun
    Liu, Xuan
    Zhu, Li
    SCIENTIFIC WORLD JOURNAL, 2014,
  • [3] A Novel Nonlinear Filter for Initial Alignment in Strapdown Inertial Navigation System
    Xiang Li
    Liu Yu
    Su Baoku
    Jiang Xiaoxiong
    2008 2ND INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1 AND 2, 2008, : 820 - 825
  • [4] APPLICATION OF OPTIMAL-CONTROL TO INITIAL ALIGNMENT OF STRAPDOWN INERTIAL NAVIGATION SYSTEM (INS)
    LIU, WP
    HIGASHIGUCHI, M
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 1989, 32 (96) : 67 - 78
  • [5] A fast robust Kalman filter for initial alignment of strapdown inertial navigation system
    Li, Xuyou
    Meng, Qingwen
    Liu, Meng
    Guo, Yanda
    OPTIK, 2021, 237
  • [6] Application of H∞ filtering in the initial alignment of strapdown inertial navigation system
    Yu Fei
    Sun Feng
    Journal of Marine Science and Application, 2005, 4 (1) : 50 - 53
  • [7] Application of H∞ filtering in the initial alignment of strapdown inertial navigation system
    YU Fei and SUN Feng School of Automation
    Journal of Marine Science and Application, 2005, (01) : 50 - 53
  • [8] An initial alignment method for strapdown gyrocompass based on gravitational apparent motion in inertial frame
    Liu, Xixiang
    Xu, Xiaosu
    Zhao, Yu
    Wang, Lihui
    Liu, Yiting
    MEASUREMENT, 2014, 55 : 593 - 604
  • [9] Application of Adaptive Kalman Filter Technique in Initial Alignment of Strapdown Inertial Navigation System
    Huang Chunmei
    Su Wanxin
    Liu Peiwei
    Ma Minglong
    PROCEEDINGS OF THE 29TH CHINESE CONTROL CONFERENCE, 2010, : 2087 - 2090
  • [10] Inertial-frame-based Coarse Initial Alignment for Marine Strapdown Inertial Navigation System Using Wavelet De-noising
    Guan Dongxue
    Cheng Jianhua
    Zhao Lin
    Fei Zaihui
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 5596 - 5600