Research Article
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 |
| | 1.598075 | rad/s | | 0.52089 | rad/s | | 1.72514652738 | rad/s2 | | 22.61196 | rad/s2 | | 0.485 | | | 9.972922 | — | | 11.964 | | | 84.5 | m/s | | 9.81 | m/s2 | | 5.26416 | rad/s2 | | 0.029 | — | — | — | — |
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