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

Figure 6

Oscillations when 𝛿^𝑒=−0.04678[rad]=−2.681^∘→𝛿^𝑒=0.048[rad]=2.751^∘ and the starting point is 𝛼^1=0.086974288[rad]=4.985^∘; 𝑞^1=0[rad/sec]; 𝜃^1=0.1593297[rad]=9.133^∘.

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(b)

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