Automatic estimation of inertial navigation system errors for global positioning system outage recovery

被引:16
|
作者
Hasan, A. M. [1 ]
Samsudin, K. [1 ]
Ramli, A. R. [2 ]
Azmir, R. S. [3 ]
机构
[1] Univ Putra Malaysia, Dept Comp & Commun Syst, Comp Syst Res Grp, Serdang, Malaysia
[2] Univ Putra Malaysia, Inst Adv Technol, Intelligent Syst & Robot Lab, Serdang, Malaysia
[3] Univ Putra Malaysia, Res Ctr Excellence, Wireless & Photon Networks WiPNET, Serdang, Malaysia
关键词
global positioning system; inertial navigation system; adaptive neuro-fuzzy inference system; genetic neuro-fuzzy inference system; intelligent navigator; windowing method; KALMAN FILTER; INTEGRATION;
D O I
10.1243/09544100JAERO731
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article presents an alternative approach of solving global positioning system (GPS) outages without requiring any prior information about the characteristics of the inertial navigation system (INS) and GPS sensors. INS can be used as a standalone system to bridge the outages during GPS signal loss. Kalman filter (KF) is widely used in INS and GPS integration to present a forceful navigation solution by overcoming the GPS outage problems. Unfortunately, KF is usually criticized for working under predefined models and for its observability problem of hidden state variables, sensor dependency, and linearization dependency. This approach utilizes a genetic neuro-fuzzy system (GANFIS) to predict the INS position and velocity errors during GPS signal blockages suitable for real-time application. The proposed model is able to deal with noise and disturbances in the GPS and INS output data in different dynamic environments compared to other traditional filtering algorithms such as the neural network and neuro fuzzy. Real field test results using the micro-electro-mechanical system grade inertial measurement unit with an integrated GPS shows a significant improvement obtained from the integrated GPS/INS system using the GANFIS module compared to traditional methods such as Kalman filtering, particularly during long GPS satellite signal blockage.
引用
收藏
页码:86 / 96
页数:11
相关论文
共 50 条
  • [41] Global positioning system integrated navigation and attitude determination system (GINAS)
    Lucas, R.
    Martinez, M.A.
    Martin-Neira, M.
    Signal Processing - Theories and Applications, 1990,
  • [42] Inertial Navigation System for an Automatic Guided Vehicle with Mecanum Wheels
    Kim, Jungmin
    Woo, Seungbeom
    Kim, Jaeyong
    Do, Joocheol
    Kim, Sungshin
    Bae, Sunil
    INTERNATIONAL JOURNAL OF PRECISION ENGINEERING AND MANUFACTURING, 2012, 13 (03) : 379 - 386
  • [43] Inertial navigation system for an automatic guided vehicle with Mecanum wheels
    Jungmin Kim
    Seungbeom Woo
    Jaeyong Kim
    Joocheol Do
    Sungshin Kim
    Sunil Bae
    International Journal of Precision Engineering and Manufacturing, 2012, 13 : 379 - 386
  • [44] APPLICATION OF THE GLOBAL POSITIONING SYSTEM FOR HERMES RENDEZVOUS NAVIGATION
    AMBROSIUS, BAC
    HESPER, ET
    WAKKER, KF
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1993, 16 (01) : 197 - 205
  • [45] TRILATERATION AND EXTENSION TO GLOBAL POSITIONING SYSTEM NAVIGATION.
    Fang, Bertrand T.
    1600, (09):
  • [46] GLOBAL POSITIONING SYSTEM SURFACE NAVIGATION ACCURACY STUDY
    DUVEN, DJ
    ARTIS, DA
    MARINE GEODESY, 1985, 9 (02) : 145 - 173
  • [47] Global positioning system interference and navigation tool (GIANT)
    Green, Gary L.
    Wollam, Jon
    IEEE Aerospace Applications Conference Proceedings, 1999, 5 : 29 - 38
  • [48] GEOMETRIC DILUTION OF PRECISION IN GLOBAL POSITIONING SYSTEM NAVIGATION
    FANG, BT
    JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (01): : 92 - 94
  • [49] SEQUENTIAL RANGE NAVIGATION FOR NAVSTAR GLOBAL POSITIONING SYSTEM
    BUONAGURO, A
    MCCASKILL, TB
    BUISSON, JA
    REPORT OF NRL PROGRESS, 1975, (MAY): : 34 - 34
  • [50] Global Navigation Satellite System Precise Positioning Technology
    Kubo, Nobuaki
    IEICE TRANSACTIONS ON COMMUNICATIONS, 2024, E107B (11) : 691 - 705