Matlab: Find the errors - debug the given code. Follow the instructions of a. b. c. at the bottom. Provide a clear explanation of both plots and a. and b. as well as comments throughout your work process. Numerical Methods for Engineers - 7th edition (this is a problem given seperate from the book) If you can't solve the entire thing just try your best on both of the plots

A MATLAB script is provided below, which does the following: a. Defines all problem parameters. For this problem, the drag coefficient is set to c -12.5 kg/s and the parachutist's mass m is equal to 75Kg. b. Plots the exact, analytical solution for this problem over the range t 0 tot 60 s The algorithm below has several errors. Correct them and create one plot showing the analytical solutions function FDD parachutist close all define constants 12.5 [kg/s m 75 g 10 Sm/s 2 t0 60 tend step 1; dt in [s] analytical solution t to tend; u m/c* exp (c/m) *t)) splot analytical solution figure plot (t u, r') hold on ylabel Time (S Font Weight bold') label Velocity v (t) Font Weight 'bold') numerical solution [velocity] fdd (step, tend, g, c) splot numerical solution plot (velocity 1) velocity 2) g title Parachutist Example Terminal Velocity Exact Vs Numerical r Font Weight r bold') legend (I' Numer Exact j)