Modeling of dynamical systems is the primary attraction of many researchers from many decades. In this paper the modeling of Missile Launch Vehicle (MLV) System is reported. The detailed model analysis of the considered system is also reported. The model equations are found by using Euler–Lagrangian equation and comment on stability is given by using Lyapunove’s theorem.
CITATION STYLE
Singh, A. P., & Agrawal, H. (2016). On modeling and analysis of launch vehicle system. In Lecture Notes in Electrical Engineering (Vol. 396, pp. 273–279). Springer Verlag. https://doi.org/10.1007/978-81-322-3589-7_30
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