An Overview of Initial Alignment Methods in Inertial Navigation

GUO Yinjing; YANG Wenjian; LIU Zhen

doi:10.3969/j.issn.1671-637x.2020.12.014

[4] GENG Y R, WANG J L.Adaptive estimation of multiple fading factors in Kalman filter for navigation applications［J］.GPS Solutions, 2008, 12(4):273-279.

[5] CHEN B, LIU Z Z.Voxel-optimized regional water vapor tomography and comparison with radiosonde and numerical weather model［J］.Journal of Geodesy, 2014, 88(7):691-703.

[6] CHANG G B.Kalman filter with both adaptivity and robustness［J］.Journal of Process Control, 2014, 24(3):81-87.

[7] CHANG G B.Robust Kalman filtering based on Mahalanobis distance as outlier judging criterion［J］.Journal of Geodesy, 2014, 88(4):391-401.

[14] ZHOU B C, CHENG X H.Robust UKF algorithm in SINS initial alignment［J］.Journal of Southeast University(English Edition), 2011, 27(1):56-60.

[15] CHANDRA K P B, GU D W, POSTLETHWAITE I.A cubature H∞ filter and its square-root version［J］.International Journal of Control, 2014, 87(4):764-776.

[16] CHANG L B, HU B Q, LI A, et al.Transformed unscented Kalman filter［J］.IEEE Transactions on Automatic Control, 2013, 58(1):252-257.

[17] YANG B, XU X S, ZHANG T, et al.Novel SINS initial alignment method under large misalignment angles and uncertain noise based on nonlinear filter［J］.Mathematical Problems in Engineering, 2017(4):1-14.

[18] MENG Y, GAO S S, ZHONG Y M, et al.Covariance matching based adaptive unscented Kalman filter for direct filtering in INS/GNSS integration［J］.Acta Astronautica, 2016, 120:171-181.

[19] WANG D, LYU H F, WU J.In-flight initial alignment for small UAV MEMS-based navigation via adaptive unscented Kalman filtering approach［J］.Aerospace Science and Technology, 2017, 61:73-84.

[25] SINGH A K, BHAUMIK S.Higher degree cubature quadrature Kalman filter［J］.International Journal of Control, Automation and Systems, 2015, 13(5):1097-1105.

[26] ZHANG Y G, HUANG Y L, WU Z M, et al.Seventh-degree spherical simplex-radial cubature Kalman filter［C］//Proceedings of the 33rd Chinese Control Conference, IEEE, 2014:2513-2517.

[28] WANG W, CHEN X Y.Application of improved 5th-cubature Kalman filter in initial strapdown inertial navigation system alignment for large misalignment angles［J］.Sensors, 2018, 18(2):659.

[29] LU H, HAO S Y, PENG Z Y.Simplified 5th-degree multiple fading CKF for GPS/INS integrated navigation system［C］//Proceedings of the 37th Chinese Control Conference (CCC), IEEE, 2018:4938-4945.

[30] CHANG L B, LI J S, LI K L.Optimization-based alignment for strapdown inertial navigation system:comparison and extension［J］.IEEE Transactions on Aerospace and Electronic Systems, 2016, 52(4):1697-1713.

[31] HUANG Y L, ZHANG Y G, CHANG L B.A new fast in-motion coarse alignment method for GPS-aided low-cost SINS［J］.IEEE/ASME Transactions on Mechatronics, 2018, 23(3):1303-1313.

[32] ZHANG Q, LI S S, XU Z P, et al.Velocity-based optimization-based alignment (VBOBA) of low-end MEMS IMU/GNSS for low dynamic applications［J］.IEEE Sensors Journal, 2020, 20(10):5527-5539.

[34] XU X, XU X S, YAO Y Q, et al.In-motion coarse alignment method based on reconstructed observation vectors［J］.Review of Scientific Instruments, 2017, 88(3):035001.

[37] CHANG L B, LI Y, XUE B Y.Initial alignment for a Doppler velocity log-aided strapdown inertial navigation system with limited information［J］.IEEE/ASME Trans-actions on Mechatronics, 2017, 22(1):329-338.

[39] NOURMOHAMMADI H, KEIGHOBADI J.Integration scheme for SINS/GPS system based on vertical channel decomposition and in-motion alignment［J］.AUT Journal of Modeling and Simulation, 2018, 50(1):13-22.

[40] XU J N, HE H Y, QIN F J, et al.A novel autonomous initial alignment method for strapdown inertial navigation system［J］.IEEE Transactions on Instrumentation and Measurement, 2017, 66(9):2274-2282.

[42] XU X, XU X S, ZHANG T, et al.In-motion filter-QUEST alignment for strapdown inertial navigation systems［J］.IEEE Transactions on Instrumentation and Measurement, 2018, 67(8):1979-1993.

[44] ZHANG L, YANG C, CHEN Q W, et al.Robust H-infinity CKF/KF hybrid filtering method for SINS alignment［J］.IET Science, Measurement & Technology, 2016, 10(8):916-925.

[45] NOURMOHAMMADI H, KEIGHOBADI J.Decentralized INS/GNSS system with MEMS-grade inertial sensors using QR-factorized CKF［J］.IEEE Sensors Journal, 2017, 17(11):3278-3287.