International Journal of Mathematics and Computational Science
Articles Information
International Journal of Mathematics and Computational Science, Vol.1, No.3, Jun. 2015, Pub. Date: May 18, 2015
A Meshless Method Based on Radial Basis Functions for Approximating the Oscillations Parameters of Launching Devices During the Firing
Pages: 127-131 Views: 1314 Downloads: 469
[01] S. Sarabadan, Departeman of Mathematics, Imam Hossein University, Tehran, Iran.
[02] M. Kafili, Departeman of Mathematics, Amir Kabir University, Tehran, Iran.
The sloped rocket launch used in military forces is one of the most important kinds of defence instruments. The rockets stability during the firing path especially when they are unguided is very important for firing precision. It completely depends on the elementary conditions and oscillations when the firing. In this work, we consider this issue, modelling the problem results in a differential equations system of the second order. A meshless method based on radial basis functions (RBFs) is applied to solve the underlying system and the numerical results are presented in the figural forms.
Sloped Rocket Launching Devices, Oscillations, Radial Basis Function
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