Question: 3 . 4 PRETEND you are trying to computationally solve for the root of the Optimal Thrust equation f ( T ) = 0 using

3.4 PRETEND you are trying to computationally solve for the root of the Optimal Thrust equation f(T)=
0 using the secant method starting with the initial "bracket" T1=0.5,T2=40.
(a) Calculate the values of tol ?x and tol ?f you would use for the two convergence criteria,
TT12=T13=16.407TT13|f(xk)|,if you were to write your own secant method in MATLAB.
Now (pretend) you've completed 13 iterations for T, and the last two iterations have values T12=
16.410 and T13=16.407. For the "exact solution" use the value you got for Tin problem 3.3 above
to answer the following (and SHOW YOUR WORK!!):
(b) What is the (just plain old) error in the last iteration, T13?
(c) What is the "proxy" for the error for the last iteration?
(d) What is the "residual" error for the last iteration?
(e) Based on all your values above, explain whether the process has "converged" yet or not.|xk-xk-1| and |f(xk)|,if you were to write your own secant method in MATLAB.
Now (pretend) you've completed 13 iterations for T, and the last two iterations have values T12=
16.410 and T13=16.407. For the "exact solution" use the value you got for Tin problem 3.3 above
to answer the following (and SHOW YOUR WORK!!):
(b) What is the (just plain old) error in the last iteration, T13?
(c) What is the "proxy" for the error for the last iteration?
(d) What is the "residual" error for the last iteration?
(e) Based on all your values above, explain whether the process has "converged" yet or not.
3 . 4 PRETEND you are trying to computationally

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