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[2] Jwo, D. J., Shih, J. H., Hsu, C. S., & Yu, K. L., “development of a strapdown inertial navigation system simulation platform”, Journal of Marine Science and Technology, Vol. 22, No. 3, pp. 381-391, 2014.
[3] Zhang, W., Ghogho, M., & Yuan, B., “Mathematical model and matlab simulation of strapdown inertial navigation system”, Hindawi Publishing Corporation, Modelling and Simulation in Engineering, Vol. 2012, Article ID 264537, pp. 1-25, 2012.
[4] Titterton, D., & Weston, J. “Strapdown inertial navigation technology”, (2nd Edition), Institution of Engineering and Technology, United Kigdom, 2004.
[5] Grigorie, T. L., Lungu, M., Raluca Edu, I., & Obreja, R. “Concepts for error modeling of iniatureaccelerometers used in inertial navigation systems” annals of the university of craiova, electrical engineering _series, no. 34,; issn_ 1842-4805, 2010.
[6] Grigorie, T. L., Jula, C. C. N., & Racuciu, C. “Evaluation method of the sensors errors in an inertial navigation system”, Wseas Transactions on Circuits and Systems, issue 12, volume 7, december, issn: 1109-2734, 2008.
[7] Xu, Y., Wang, Z., & Gao, B. “Six-degree-of-freedom digital simulations for missile guidance and control” college of mechatronic engineering, north university of china, taiyuan 030051, china, received 17 march 2015; accepted 25 june, 2015.
[8] Kisabo, A. B. Adebimpe, A. F., Okwo, O. C., & Samuel, S. O. “State-space modelling of a rocket for optimal control system design” Aliyu Bhar Kisabo et al. / journal of aircraft and spacecraft technology, 2019.
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