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

Table 1

The values of the parameters used in the simplified system (3.3).

Parameter	Value	Units
𝑧𝛼	−1.598075	rad/s
𝑧𝛿𝑒	−0.52089	rad/s
𝑚𝛼	1.72514652738	rad/s^2
𝑚𝑞	−22.61196	rad/s^2
𝑎	−0.485	s^−1
𝑚𝛿𝑒	−9.972922	—
𝑎2	11.964	s^−2
𝑉	84.5	m/s
𝑔	9.81	m/s^2
𝑚̇𝛼	−5.26416	rad/s^2
𝑐2	−0.029	—
—	—	—