[Ali, J., Zhang, C.Y. (2004). Simulation algorithm for SINS axes misalignment angles through stars observation. In Proceedings of the 11th Saint Petersburg International Conference on Integrated Navigation Systems, 24-26 May 2004. Sankt-Peterburg: Elektropribor, 129-130.]Search in Google Scholar
[Leibe, C.C. (1995). Star trackers attitude determination. IEEE AES Systems Magazine, 10 (6), 10-16.10.1109/62.387971]Search in Google Scholar
[Horsfall, R.B. (1959). Celestial guidance. ARS Journal, 29, 981-988.10.2514/8.4961]Search in Google Scholar
[Eisenman, A.R., Leibe, C.C. (1997). The advancing state-of-the-art in second generation star trackers. In Calibration of AVNIR. Proc. SPIE, Vol. 3221, 524-535.10.1117/12.298121]Search in Google Scholar
[Brown, A. Moy, G. (1992). Long duration strapdown stellar-inertial navigation using satellite tracking. In IEEE Position Location and Navigation Symposium. New York: IEEE, 194-201.10.1109/PLANS.1992.185842]Search in Google Scholar
[Leibe, C.C., Dennison, E.W., Hancock, B. et al (1998). Active pixel sensor (APS) based star tracker. In IEEE Position Location and navigation Symposium. New York: IEEE, 119-127.10.1109/AERO.1998.686811]Search in Google Scholar
[Padgett, C., Delgado, K.K., Udomkesmalee, S. (1997). Evaluation of star identification techniques. Journal of Guidance, Control and Dynamics, 20 (2), 259-267.10.2514/2.4061]Search in Google Scholar
[Kosik, J. (1991). Star pattern identification aboard an inertially stabilized spacecraft. Journal of Guidance, Control and Dynamics, 20 (2), 230-235.10.2514/3.20632]Search in Google Scholar
[Wertz, J. (ed.) (1978). Spacecraft Attitude Determination and Control. Boston, MA: Reidel.10.1007/978-94-009-9907-7]Search in Google Scholar
[Shuster, M.D., Oh, S.D. (1991). Three-axis attitude determination from vector observations. Journal of Guidance, Control and Dynamics, 4 (1), 70-77.]Search in Google Scholar
[Markley, F.L. (1988). Attitude determination using vector observation and singular value decomposition. The Journal of the Astronautical Sciences, 36 (3), 245-258.]Search in Google Scholar
[Mortari, D. (1997). ESOQ: A closed form solution to the Wahba problem. Journal of the Astronautical Sciences, 45 (2), 195-204.10.1007/BF03546376]Search in Google Scholar
[Mortari, D. (1997). ESOQ2: Single point algorithm for fast optimal attitude determination. In Advances in the Astronautical Sciences, Vol. 95, Paper 97-167, 10-12 February 1997. Huntsville, AL, 817-826.]Search in Google Scholar
[Rao, G.N., Alex, T.K., Bhat, M.S. (1991). Incremental-angle and angular velocity estimation using a star sensor. Journal of Guidance, Control and Dynamics, 25 (3), 433-441.]Search in Google Scholar
[Ali, J., Fang, J.C. (2004). In-flight alignment of inertial navigation system by celestial observation technique. In Proceedings of the International Symposium on Inertial Navigation Technology and Intelligent Traffic, 15-17 October 2004. Nanjing, China.]Search in Google Scholar
[Fernandez, M., Macomber, G.R. (1962). Inertial Guidance Engineering. Prentice-Hall, Inc.]Search in Google Scholar
[Levine, S. (1995). AGARDograph on advanced astroinertial navigation systems. In AGARD-AG-331. Aerospace Navigation Systems. Research and Technology Organisation (NATO), 187-199.]Search in Google Scholar
[Kalman, R.E. (1960). A new approach to linear filtering and prediction problems. ASME Journal of Basic Engineering, 82D, 35-45.10.1115/1.3662552]Search in Google Scholar
[Quan, W., Fang, J.C. (2005). Hardware-in-the-loop simulation of celestial navigation system. In Proceedings of the 12th Saint Petersburg International Conference on Integrated Navigation Systems, 23-25 May 2005. Sankt-Peterburg: Elektropribor, 123-125.]Search in Google Scholar