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Engineering, 24.11.2020 18:40 mutesheep

An aircraft has the following short period approximation: α/δ e= (-0.746s-208.6)/(675s^2+ 1361.6s+5452.45)

Find the natural frequency, damping ratio, and the steady-state value of AOA in response to a unit step input using the final value theorem.

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An aircraft has the following short period approximation: α/δ e= (-0.746s-208.6)/(675s^2+ 1361.6s...
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