ng2003 16.61AC2-10 O 0 alpha(rad) alpha(rad) 8 gamma gamma 9R88吕吕 88 Figure 2: Step Response to 1/6 thrust perturbation- B747 at M=0. 8Spring 2003 16.61 AC 2–10 0 200 400 600 −15 −10 −5 0 5 10 15 u time 0 200 400 600 −0.02 −0.015 −0.01 −0.005 0 0.005 0.01 0.015 0.02 alpha (rad) time Step response to 1/6 thrust perturbation 0 200 400 600 0 0.02 0.04 0.06 0.08 0.1 gamma time 0 10 20 30 40 0 1 2 3 4 5 6 7 u time 0 10 20 30 40 −5 0 5 10 15 20 x 10−4 alpha (rad) time 0 10 20 30 40 0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 gamma time Figure 2: Step Response to 1/6 thrust perturbation – B747 at M=0.8