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
Posted: Fri Apr 29, 2022 10:36 am
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