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

Figure 9

A transfer between two equilibriums, which belong to 𝒫₁ (simulated in the general model): 𝛿^𝑒=−0.03866[rad]=2.216^∘→𝛿^𝑒=0.03026[rad]=1.734^∘. 𝛼^1=0.07866974[rad]=4.509^∘; 𝑞^1=0[rad/s]; 𝜃^1=−0.428832[rad]=24.582^∘→𝛼^1=0.065516[rad]=3.755^∘; 𝑞^1=0[rad/s]; 𝜃^1=−0.698066[rad]=−40.016^∘.

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