Modelling and Simulation of Surface to Surface Missile General Platform
DOI:
https://doi.org/10.3849/aimt.01236Keywords:
missile modelling, surface‐to‐surface missile, 6 degrees of freedom, equation of motion, non‐linear state space modelAbstract
In this paper, a general platform of a surface‐to‐surface missile model is presented. An accurate missile system model was made with consideration of the rigid body dynamics in space with six degrees of freedom and equation of motion starting from Newton second law to the non‐linear state space model of the missile. Computer simulations have been executed using the MATLAB / Simulink software. Verification of the system model has been made.
References
OGATA, K. Modern Control Engineering. Pearson Education, 4th ed. 2002.
LIN, C.M. and PENG, Y.F. Missile Guidance Law Design Using Adaptive Cerebellar Model Articulation Controller. IEEE Transactions on Neural Networks, 2005 vol. 16, no. 3. ISSN 1045-9227. https://doi.org/10.1109/TNN.2004.839358.
STEVENS, B. and LEWIS, F. Aircraft Control and Simulation. John Wiley, 1992.
BLAKELOCK, J.H., Automatic Control of Aircraft and Missiles. John Wiley, 2nd ed. 1991.
NELSON, R. Flight Stability and Automatic Control. McGraw‐Hill, 1989.
SIOURIS, G.M. Missile Guidance and Control Systems. Springer, 2004.
SANAGAVARAPU, S.R. et al. Mathematical Modeling and Simulation of Missile Target Engagement – 6 DOF Simulation using PN Guidance. Journal of Basic and Applied Engineering Research, 2015, vol. 2, no. 7. ISSN 2350-0077.
BARRERE, M. et al. Rocket Propulsion. Elsevier, 1960.
GOLNARAGHI, F. and KUO, B. Automatic Control Systems. Complex Variables, 2010, 9th ed. vol. 2.
TEWARI, A. Atmospheric and Space Flight Dynamics. Springer, 2007.
RAUW, M. FDC 1.2 – A Simulink Toolbox for Flight Dynamics and Control Analysis. 2001.
WANG, Q. and WANG, L.M. Research on Simulation System of Missile and Arrows Based on Unity3D. In 2nd International Conference on Computational Modeling, Simulation and Applied Mathematics (CMSAM 2017). Shenzhen, 2017.
EL-SHIKH, G.A., An Investigation into the Performance of Strapdown Inertial Navigation. Cairo: Military Technical College, 1990.
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