]>Oscillation Susceptibility Analysis of the ADMIRE Aircraft along the Path of Longitudinal Flight Equilibriums in Two Different Mathematical Models : Table 2
Table 2: The transfer periods of the transitions corresponding to the maneuver 𝜹 ′ 𝐞 = − 𝟎 . 𝟎 𝟑 𝟖 𝟔 𝟔 [ 𝐫 𝐚 𝐝 ] = − 𝟐 . 𝟐 𝟏 𝟔 ∘ → 𝜹 ′ ′ 𝐞 .
𝛿 𝑒 [rad] − 0.048 − 0.05 − 0.06 − 0.08 − 0.1 − 0.5
Transfer period [s]3331707030204