Automatic Estimation of Inertial Navigation System Errors for Global Positioning System Outage Recovery

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.

[1]  N. El-Sheimy,et al.  Automization of an INS/GPS intecrated system using genetic optimization , 2004, Proceedings World Automation Congress, 2004..

[2]  N. El-Sheimy,et al.  Online INS/GPS integration with a radial basis function neural network , 2005, IEEE Aerospace and Electronic Systems Magazine.

[3]  E. Mizutani,et al.  Neuro-Fuzzy and Soft Computing-A Computational Approach to Learning and Machine Intelligence [Book Review] , 1997, IEEE Transactions on Automatic Control.

[4]  Wei Wang,et al.  Quadratic extended Kalman filter approach for GPS/INS integration , 2006 .

[5]  Franco Persiani,et al.  Multiobjective wing design using genetic algorithms and fuzzy logic , 2004 .

[6]  F. Gagnon,et al.  Fuzzy corrections in a GPS/INS hybrid navigation system , 2004, IEEE Transactions on Aerospace and Electronic Systems.

[7]  Robert Sutton,et al.  Adaptive tuning of a Kalman filter via fuzzy logic for an intelligent AUV navigation system , 2004 .

[8]  D. K. Mynbaev Errors of an inertial navigation unit caused by ring laser gyros errors , 1994, Proceedings of 1994 IEEE Position, Location and Navigation Symposium - PLANS'94.

[9]  Martin P. Mintchev,et al.  Accuracy limitations of FOG-based continuous measurement-while-drilling surveying instruments for horizontal wells , 2002, IEEE Trans. Instrum. Meas..

[10]  Li-Xin Wang,et al.  Adaptive fuzzy systems and control - design and stability analysis , 1994 .

[11]  Naser El-Sheimy,et al.  Improving INS/GPS Positioning Accuracy During GPS Outages Using Fuzzy Logic , 2003 .

[12]  Mohinder S. Grewal,et al.  Global Positioning Systems, Inertial Navigation, and Integration , 2000 .

[13]  Abdul Rahman Ramli,et al.  Comparative Study on Wavelet Filter and Thresholding Selection for GPS/INS Data Fusion , 2010, Int. J. Wavelets Multiresolution Inf. Process..

[14]  John Weston,et al.  Strapdown Inertial Navigation Technology , 1997 .

[15]  Abhishek Halder,et al.  Fuzzy state noise-driven Kalman filter for sensor fusion , 2009 .

[16]  Faroog Ibrahim,et al.  DGPS/INS Integration Using Linear Neurons , 2000 .

[17]  P. Vanicek,et al.  DOES A NAVIGATION ALGORITHM HAVE TO USE A KALMAN FILTER , 1999 .

[18]  Mohammed Tarbouchi,et al.  Real-Time Implementation of INS/GPS Data Fusion Utilizing Adaptive Neuro-Fuzzy Inference system , 2005 .

[19]  Willem H. Steyn,et al.  Kalman filter configurations for a low-cost loosely integrated inertial navigation system on an airship , 2008 .

[20]  A. Noureldin,et al.  Bridging GPS outages using neural network estimates of INS position and velocity errors , 2006 .

[21]  Naser El-Sheimy,et al.  A neuro-wavelet method for multi-sensor system integration for vehicular navigation , 2004 .

[22]  Naser El-Sheimy,et al.  Improving INS/GPS Navigation Accuracy through Compensation of Kalman Filter Errors , 2006, IEEE Vehicular Technology Conference.

[23]  Guoqiang Mao,et al.  Design of an Extended Kalman Filter for UAV Localization , 2007, 2007 Information, Decision and Control.

[24]  Michael Forrest,et al.  An Inertial Navigation Data Fusion System employing an Artificial Neural Network as the Data Integrator , 2000 .

[25]  Antonios Tsourdos,et al.  Unmanned aerial vehicle navigation and mapping , 2008 .