Transfer Alignment for MEMS Integrated Navigation System Based on H∞ Filter

被引:0
作者
Zhang Xingzhi [1 ]
He Kunpeng [1 ]
Wang Chenyang [1 ]
机构
[1] Harbin Engn Univ, Coll Automat, Harbin 150001, Peoples R China
来源
MECHANICAL DESIGN AND POWER ENGINEERING, PTS 1 AND 2 | 2014年 / 490-491卷
关键词
integrated navigation system; transfer alignment; H-infinity filter; Kalman filter;
D O I
10.4028/www.scientific.net/AMM.490-491.886
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The transfer alignment of strapdown inertial units were proposed that use the H-infinity filter to estimate the misalignment of the slave INS (inertial navigation system) relative to the master INS. Characteristics of the H-infinity filter in transfer alignment were studied in detail by checking digital simulation results obtained by using the H-infinity and Kalman filters. The results shows that the misalignment angle obtained with the H-infinity filter converge faster and closer to the exact values than do those obtained with the Kalman filter. The H-infinity filter is more robust than the Kalman filter in transfer alignment for MEMS integrated navigation system.
引用
收藏
页码:886 / 890
页数:5
相关论文
共 6 条
  • [1] [Anonymous], 2000, AIAA ED SERIES
  • [2] DMITRIYEV S.P., 1997, IEEE T AES, V33
  • [3] Optimising the transfer alignment of weapon INS
    Groves, PD
    [J]. JOURNAL OF NAVIGATION, 2003, 56 (02) : 323 - 335
  • [4] SATO Tadanobu, STRUCTURAL ENG EARTH, V15
  • [5] Central Difference Particle Filter Applied to Transfer Alignment for SINS on Missiles
    Wang, Yafeng
    Sun, Fuchun
    Zhang, Youan
    Liu, Huaping
    Min, Haibo
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2012, 48 (01) : 375 - 387
  • [6] YUE Xiaokui, 2004, CHINESE J AERONAUT, V17, P201