Using Matlab solve the following problem.

x=[0.0,8.652,16.58,30.21,46.78,58.79,67.44,79.26,89.43,101.59,108.99,119.76,130.50];

in this case X is the Time

y=[38.501,3896.9,6978.0,11297.9,14778.5,16027.4,16274.4,15713.5,14407.3,11643.3,9287.4,5173.1,124.7];

in this case Y is the height in ft

h(t)= -3.62t^2+473.0t+38.2

I have laid out the steps as to how this should be solved.

% Create row vectors for both the measured time and height/altitude % given in Table 1. Suppress the output to the command window. X=[0.0,8.652,16.58, 30.21,46.78,58.79,67.44,79.26,89.43, 101.59, 108.99, 119.76, 130.50); y=[38.501,3896.9,6978.0, 11297.9, 14778.5,16027.4,16274.4, 15713.5, 14407.3, 11643.3,9287.4,5173.1, 124.7); % % (2) % Create a row vector for time from 0.0 to 135.0 that has increments of 1.5 % seconds. Suppress the output to the command window. % % (3) % Evaluate the predefined flight profile h(t) given above using the time % vector created in the previous step. Use element-by-element math and % suppress output to the command window. %% (4) % Create a plot of height versus time for both the measured and specified % flight profiles. Plot both lines on the same axis. Include a descriptive % title, axis labels, and a legend in the plot. %% (5) % Evaluate the predefined flight profile h(t) ONLY at the time values % recorded during flight. Use element-by-element computations and suppress $output to the command window. %% (6) % Compute the percent error between the measured height and the % predefined profile. Use element-by-element computations and DO NOT