Research Article

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

Figure 1

The 𝛼 1 ( 𝛿 𝑒 ) and 𝛼 2 ( 𝛿 𝑒 ) coordinates of the equilibriums on the manifold 𝑉 .
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