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 and for c.

AMATLAB 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. Plots the exact, analytical solution for this problem over the range 0 tot 60 s. The algorithm below has several errors. Correct them and create one plot showing the analytical solutions function EDD parachutist close all define constants g 10 in/s 21 to tend 60 step l dt in analytical solution -t 0:tend. (l-exp plot analytical solution figure plot (t hold ylabel Time (s Font Weight bold xlabel. velocity v (t) Fontieight bold') numerical solution velocity] f dd (step, tend, g, 2 plot numerical solution plot (velocity 1) r velocity 21 'g') title Parachutist Example Terminal Velocity Exact Va Numerical Font weight bold. legend It Nume Exact 'J) tunction Lvelocity toid step,tend, g, c,m rinite divided dirrerence approxima t1 on velocity 10,01: for i 1:h: tend start for loop from 1 velocity [velocity li,v)] ena end