Simulation of Rocket Recovery

The objective of the project is to simulate the trajectories of a rocket as it descends
onto a mountainous terrain. Along the trajectories, the motion of the rocket is assumably
in
uenced by propulsion, air drag on the rocket body, gravity, wind advection, and the
parachutes during recovery. You will simulate and analyze various launches to examine how
the deployment of the parachutes aects the
ight dynamics.