Linearized In-Motion Alignment for a Low-Cost INS

An accurately linearized in-motion alignment with a large heading error is proposed for a low-cost inertial navigation system with the aiding of global positioning system. The linearization is designed for both the coarse and the fine stages in the local level frame. A criterion is constructed to determine the time to switch the alignment from the coarse stage to the fine one automatically. A vehicle test demonstrates that the proposed alignment converges fast and accurately.

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

[2]  Jinling Wang,et al.  A Novel Initial Alignment Scheme for Low-Cost INS Aided by GPS for Land Vehicle Applications , 2010, Journal of Navigation.

[3]  Donghua Zhou,et al.  Adaptive In-Flight Alignment of INS/GPS Systems for Aerial Mapping , 2018, IEEE Transactions on Aerospace and Electronic Systems.

[4]  Hugh F. Durrant-Whyte,et al.  Development of a nonlinear psi-angle model for large misalignment errors and its application in INS alignment and calibration , 1999, Proceedings 1999 IEEE International Conference on Robotics and Automation (Cat. No.99CH36288C).

[5]  Burak H. Kaygisiz,et al.  In-motion Alignment of a Low-cost GPS/INS under Large Heading Error , 2015 .

[6]  Zhao Pengfei,et al.  SINS In-Motion Alignment for Initial Attitude Uncertainty , 2015, 2015 Fifth International Conference on Instrumentation and Measurement, Computer, Communication and Control (IMCCC).

[7]  Jinling Wang,et al.  Effective Adaptive Kalman Filter for MEMS-IMU/Magnetometers Integrated Attitude and Heading Reference Systems , 2012, Journal of Navigation.

[8]  Myeong-Jong Yu,et al.  Equivalent nonlinear error models of strapdown inertial navigation system , 1997 .

[9]  Xiaoji Niu,et al.  Civilian Vehicle Navigation: Required Alignment of the Inertial Sensors for Acceptable Navigation Accuracies , 2008, IEEE Transactions on Vehicular Technology.

[10]  Hyun-Su Hong,et al.  Performance improvement of in-flight alignment for autonomous vehicle under large initial heading error , 2004 .

[11]  B. M. Scherzinger Inertial navigator error models for large heading uncertainty , 1996, Proceedings of Position, Location and Navigation Symposium - PLANS '96.

[12]  T.M. Pham Kalman filter mechanization for INS airstart , 1992, IEEE Aerospace and Electronic Systems Magazine.

[13]  Tong Cao,et al.  A Robust Self-Alignment Method for Ship's Strapdown INS Under Mooring Conditions , 2013, Sensors.

[14]  Jang Gyu Lee,et al.  Comparison of SDINS in-flight alignment using equivalent error models , 1999 .

[15]  Itzik Klein,et al.  Analytic Evaluation of Fine Alignment for Velocity Aided INS , 2018, IEEE Transactions on Aerospace and Electronic Systems.

[16]  Robert M. Rogers IMU IN-MOTION ALIGNMENT WITHOUT BENEFIT OF ATTITUDE INITIALIZATION , 1997 .

[17]  Yuanxin Wu,et al.  A New Technique for INS/GNSS Attitude and Parameter Estimation Using Online Optimization , 2014, IEEE Transactions on Signal Processing.