I need a MATLAB code

Consider the McDonnell Douglas F-4C data on page 675-676 (Introduction to Aircraft Flight Mechanics, T. R. Yechout, 2014) for flight condition H = 35,000 ft, V = 584 ft/s. Also consider the pure pitching model indicated below. (t) Mg.(t) - Moo(t) = Mse de(t) with Mo = Mg = -0.307 1/s Me = Ma = -1.927 1/s2 Mp = M = -4.90 1/s2 a) Two-Step Input Validation (50 Points) For the elevator two-step input signal indicated below, validate your computer simulated response by matching the given e(t) vs. t plot and the given condition for e(t) using a time step of At = 0.01 s. 5-6 deg for 0 St