Write a Matlab code that uses the ODE45 function to compute the T-B angles [OA,,[T with respect to time t E [0,3010 for this aircraft. For this problem, consider the following 2 cases: . [0(0), 0(0), ii,(0)1T = [0,0, OIT, w(0) = [0, 0,10]T Hz, and Ali(1) = (0,0,01T N • m, where denotes the body fixed frame, t E [0, 301s; • [0(0), 0(0),4 (0)[T = [7/4,r/3, OIT, w(0) = [-1, 0,10]T Hz, and Ali = [0, 1, OIT N • E [0,30]s. Hint: Differential equations for both the T-B angles [OA 4d• and angular velocities [p, q,r]T need to be integrated by ODE45 to get T-B angles with respect to time. Instructions: To submit your solution to the problem, plot the Euler angles and the components of the angular velocity separately and print all your plots. Write sour Matlab code so that all plots are automatically generated by executing the code.
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