Using matlab, write a code that determines the launch angle needed to hit a target 9.4 miles away. Aerodynamic drag is calculated by Fd=0.5*rho*A*Cd*V^2

given: projectile's diameter D=6.1 inches

projectile weight 44 pounds

rail exit velocity= Mach 7

Determine (use a 0.001 second step size in your all simulations) the maximum altitude and velocity. the launch angle, in degrees, needed to hit a target 9.4 miles away the velocity at impact Plot the trajectory on an x-y plot the trajectory on anx-y plot. the acceleration g's, velocity (mph), Mach number, and drag coefficient versus time