[1] Jiang, Y.F. and Lin, Y.P.,"Error Estimation of INS Ground Alignment through Observability Analysis,"IEEE Trans. on Aerospace and Electronic Systems,Vol.28, No.3, 1992,pp. 92–97.
[2]
Feng,
Y.
F., "Analysis on Observability of SINS Multi-Position Alignment Based on Singular Value Decomposition,"
Journal of Chinese Inertial Technology, Vol. 22, No.5, 2008, pp.38-43.
[3]
Wang,
Y.D.,
Liu,
W., "Application of Local Observability Theory in Rapid Transfer Alignment of INS,"
Journal of Chinese Inertial Technology, Vol. 36, No.2, 2007, pp. 11-16.
[4] Zhou, D. H. and Guohui, H. H.,"Application of Two Stage Decoupled Kalman Filtering to the Self Contained Calibration and Alignment of Platform Inertial Navigation System,"Harbin Institute of Technology, Vol. 16, No.7,1996, pp. 42-49.
[5] Hu, C., Zheng, J. and Li, J., "Rapid Self-Calibration for Small Gesture Inertial Platform beforeLaunch,"Journal of Chinese Inertial Technology, Vol. 19, No. 7, 2007,pp. 46-52.
[6] Yong, J. S., Jeong, H. P. and Cheon,J. K., "Fast Calibration Technique for a Gimballed Inertial Navigation System,"ICAS Congress, 2002.
[7] Bar-Itzhack, I.Y. and Bermant, N., "Control Theoretic Approach to Inertial Navigation Systems,"Journal of Guidance, Control, and Dynamics,Vol. 11, No.8,1988, pp. 237–245.
[8] Wu Y., Wu M., Hu X., Hu D., "Self-Calibration for Land Navigation Using Inertial Sensors and Odometer: Observability Analysis,"AIAA Guidance, Navigation and Control Conference, Chicago, Illinois, USA, 2009.
[9]XJiang V. XLin, V. "Error Estimation of INS Ground Alignment through Observability Analysis,"IEEE Trans. on Aerospace and Electronic Systems,Vol.28, No.3, 1992, pp. 92–97.
[10] Schweppe, F. C., Uncertain Dynamic System, Prentice-Hall, 1990, pp. 129-155.
[11]Yaghini, M. and Akhavan, M., Heuristic Optimization Algorithm, Amirkabir University, Scientific Information Database, 2003(In Persian).
[12] Meleshco, V.V., Initial Alignment in Inertial Navigation System, Kornichok Kief, 1999, pp. 45-72 (In Russian).
