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].

Parameter	Value
	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