]>Oscillation Susceptibility Analysis of the ADMIRE Aircraft along the Path of Longitudinal Flight Equilibriums in Two Different Mathematical Models : Figure 1
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Figure 1: The 𝛼 1 ( 𝛿 𝑒 ) and 𝛼 2 ( 𝛿 𝑒 ) coordinates of the equilibriums on the manifold ℳ 𝑉 .