Quaternion optimization based in-flight calibration approach for POS

Position and Orientation System (POS) is a key technology which provides motion compensation information for imaging sensor in airborne remote sensing. But precision of POS is degraded by gyroscope bias excursion as time flows, in-flight calibration is the most convenient way to solve this problem to the users, but the existing methods are mostly based on kalman filter, the effect of them to estimate the bias error is unpractical as affected severely by GPS measurement error and model error. On the basis of quaternion optimization based in-flight alignment approach, a novel airborne POS in-flight calibration approach based on quaternion optimization is devised in this paper, which adds the factor of attitude error promulgation by gyroscope bias error into the algorithm and gyroscope bias error is recognized by parse analysis. Flight experiments demonstrate that with the proposed algorithm the gyroscope bias error can be recognized in acceptable precision.

[1]  Fang Jiancheng,et al.  Study on Innovation Adaptive EKF for In-Flight Alignment of Airborne POS , 2011, IEEE Transactions on Instrumentation and Measurement.

[2]  Jang Gyu Lee,et al.  A leveling algorithm for an underwater vehicle using extended Kalman filter , 1998, IEEE 1998 Position Location and Navigation Symposium (Cat. No.98CH36153).

[3]  G. Wahba A Least Squares Estimate of Satellite Attitude , 1965 .

[4]  D. Hu,et al.  Optimization-based alignment for inertial navigation systems: Theory and algorithm , 2011 .

[5]  Xinlong Wang,et al.  An intelligentized and fast calibration method of SINS on moving base for planed missiles , 2009 .

[6]  Xinlong Wang Fast alignment and calibration algorithms for inertial navigation system , 2009 .

[7]  O.A. Stepanov,et al.  Nonlinear filtering methods application in INS alignment , 1997, IEEE Transactions on Aerospace and Electronic Systems.

[8]  R. Weinman,et al.  Development, performance assessment, and verification of a calibration and alignment technique for a precision IMU , 1981 .

[9]  Fang Jiancheng,et al.  Quaternion-Optimization-Based In-Flight Alignment Approach for Airborne POS , 2012 .

[10]  T. M. Pham Kalman filter mechanization for INS airstart , 1992 .

[11]  M. Mostafa,et al.  DIRECT POSITIONING AND ORIENTATION SYSTEMS HOW DO THEY WORK? WHAT IS THE ATTAINABLE ACCURACY? , 2001 .

[12]  I. Y. Bar-Itzhack,et al.  Minimal order time sharing filters for INS in-flight alignment , 1982 .

[13]  Jiancheng Fang,et al.  Predictive Iterated Kalman Filter for INS/GPS Integration and Its Application to SAR Motion Compensation , 2010, IEEE Transactions on Instrumentation and Measurement.

[14]  M. S. Grewal,et al.  Application of Kalman filtering to the calibration and alignment of inertial navigation systems , 1990, 29th IEEE Conference on Decision and Control.

[15]  Jeffrey K. Uhlmann,et al.  Unscented filtering and nonlinear estimation , 2004, Proceedings of the IEEE.

[16]  Li Ji INS Nonlinear Alignment with Large Azimuth Misalignment Angle Using Predictive Filter , 2003 .

[17]  Jiancheng Fang,et al.  Analyses and Comparisons of Some Nonlinear Kalman Filters in POS for Airborne SAR Motion Compensation , 2007, 2007 International Conference on Mechatronics and Automation.

[18]  Kwangjin Kim,et al.  In-Flight Alignment Algorithm based on Non-Symmetric Unscented Transformation , 2006, 2006 SICE-ICASE International Joint Conference.

[19]  A. Jackson,et al.  Continuous calibration and alignment techniques for an all-attitude inertial platform , 1973 .