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

Figure 4

A transfer of an equilibrium, which belongs to 𝒫₂ into an equilibrium, which belongs to 𝒫₁ (simulated in the simplified model): 𝛿^𝑒=−0.03866[rad]=2.216^∘→𝛿^𝑒=0.03026[rad]=1.734^∘. 𝛼^2=0.064883[rad]=3.719^∘; 𝑞^2=0[rad/s]; 𝜃^2=0.7674624[rad]=43.994^∘→𝛼^1=0.065516[rad]=3.755^∘; 𝑞^1=0[rad/s]; 𝜃^1=−0.6980667[rad]=−40.016^∘ instead of 𝛼^2=0.064883[rad]=3.719^∘; 𝑞^2=0[rad/s]; 𝜃^2=0.7674624[rad]=43.994^∘→𝛼^2=0.046845[rad]=2.685^∘; 𝑞^2=0[rad/s]; 𝜃^2=1.03669718[rad]=59.428^∘.

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