Mathematical model: A simple mathematical model that describes the equations of motion is given as: m ca(2 2 = 0 my +cay(2 2)i = (1) + (2) = -mg – Missile mass = 800 (kg) – Spatial horizontal distance traveled Spatial vertical distance traveled Aerodynamic drag coefficient = 0.15 (-) where: m _ y – __ Gravitational acceleration = 9.81 (m/s^2) g Solving this system of ODES results in obtaining the distance and velocity of the object in horizontal and vertical directions Assignments: 1. Analytical solutions: Derive the state-space representation for the problem. a.
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