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dentify the inputs and formulas needed so that given the velocities and angular orientation at the velocities and orientationt t = . . of the

dentify the inputs and formulas needed so that given the velocities and
angular orientation at the velocities and orientationt t=
.
.
of the aircraft can
be determined for
2 Write a MATLAB program that utilizes the formulas derived.
Submit a single multipage pdf document with your formulas and an .m file
with your program.
t t

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