Please answer in MATLAB

3.Simple Rocket Consider the flight path of a rocket flying in 2D. Use the same model as presented in Wednesdays video, which includes a drag force as well as the force of gravity, but include the following effects:

The mass of the rocket decreases over time at a constant rate, (read as m dot). This means the mass of the rocket, is given by ()=₀, where ₀ is the initial mass

There is a constant Thrust force(), oriented parallel to the velocity vector For this problem, use =0.1,=0.12,=1/³,=1000,

₀=30,=0.5/.

Using ODE45, solve for the rockets trajectory from t = 0 to t = 20s, and use an initial condition of ₀=₀=0, ₀=0.01/, ₀=1/

Save the vector representing ()on HW7_10.dat, and the vector representing ()on HW7_11.dat.

Also, plot the trajectory of the rocket, ()vs. ()