USING A MODIFIED EULER'S MODEL FOR DETERMINING A BALLISTIC TRAJECTORY OF AN ANTIHAIL ROCKET: THEORETIC AND SOFTWARE SOLUTION
 

Ljubomir Matić

Apstrakt
The topic of this work is a descritption of a mathematical model and a software solution which can be used to calculate antihail rocket trajectories in real meteorological conditions. The software solutions enables efficient and cost-effective commanding of dislocated antihail rocket „units“ at given time intervals.

Key words:
antihail rocket, ballisticd trajectory, rocket trajectory, exterior ballistics, Euler's method, Euler's equations, Runge-Kutt method, effects of atmospheric conditions, motion thorugh the atmosphere, mathematicall model, software solution, software.