International Journal of Aerospace Engineering / 2018 / Article / Tab 1

Research Article

Adaptive Differential Thrust Methodology for Lateral/Directional Stability of an Aircraft with a Completely Damaged Vertical Stabilizer

Table 1

The nominal (undamaged) aircraft data [21, 22].

ParameterValue

5500
196
27.3
69.83
−0.160
−0.340
0.130
0.013
0.008
0.160
−0.026
−0.28
0.0018
−0.100
−0.90
0
0
0
0.120

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