For you MATLAB lovers! Need helping generating this.

Find the velocity, pitch, and angle of attack time responses of your aircraft when subjected to the following elevator inputs.

U = 673 ft/s Alpha = 2.5 deg Theta = 2.5 deg

1. Step input of 1 degree 2. Step input of-1 degree 3. Step input of -2 degrees 4. Doublet of 2 degrees that lasts 2 seconds and starts at 1 second 5. Doublet of 2 degrees that lasts 8 seconds and starts at 1 second Remember that the transfer functions must use radians and the velocity is in fti's. Also, remember that the transfer functions provide the change in the values, so your results must be added to the initial cruise values. For each input plot the following four things: input vs time, angle of attack (degrees) vs time, velocity vs time, and pitch angle (degrees) vs time. u(s) 8 e (S) The functionrelates the forward velocity of the aircraft to a change in the elevator a(s) angle, the function relates the angle of attack of the aircraft to a change in the elevator (s) angle and the function relates th relates the pitch angle of the aircraft to a change in the elevator angle