The block diagram of a rate loop for a missile autopilot is shown in Figure CP5.8. Using the analytic formulas for second-order systems, predict Mpt, Tp, and Ts for the closed-loop system due to a unit step input. Compare the predicted results with the actual unit step response obtained with the step function. Explain any differences.
Figure CP5.8
A missile rate loop autopilot.

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Missile dynamics 100(s + 1) (s2 2s00) Controller iAn+ Desired ノート 0.1 +- ttti Actual ratc ratc