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

Figure 7

Resetting 𝛿_𝑒 from 𝛿^𝑒=0.048[rad]=2.751^∘<𝛿_𝑒 to 𝛿^𝑒=−0.04678[rad]=−2.681^∘ after 3000 [s] of oscillations a stable equilibrium is recovered.

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(b)

(c)