Oscillation Susceptibility Analysis of the ADMIRE Aircraft along the Path of Longitudinal Flight Equilibriums in Two Different Mathematical Models

Table 2

The transfer periods of the transitions corresponding to the maneuver 𝜹^′_𝐞=−𝟎.𝟎𝟑𝟖𝟔𝟔[𝐫𝐚𝐝]=−𝟐.𝟐𝟏𝟔^∘→𝜹^′′_𝐞.

𝛿^𝑒[rad]	−0.048	−0.05	−0.06	−0.08	−0.1	−0.5
Transfer period [s]	333	170	70	30	20	4