4.63. Consider the model of an airplane discussed in Problem 4.49, Figure P4.49 modeled by 3000 0 0 0 12,000 0 0 3000 13

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4 63 Consider The Model Of An Airplane Discussed In Problem 4 49 Figure P4 49 Modeled By 3000 0 0 0 12 000 0 0 3000 13 1 (57.9 KiB) Viewed 23 times

4.63. Consider the model of an airplane discussed in Problem 4.49, Figure P4.49 modeled by 3000 0 0 0 12,000 0 0 3000 13,455 -13,455 0 X + -13,455 26,910 -13,455 x = 0 -13,455 13,455 subject to the initial conditions x(0) = [0.02 0 0]'m and x(0) = 0. (a) Calculate the response assuming that the damping provided by the wing rotation is Si 0.01 in