Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control

Table 1

Performance parameters.

𝜌^𝜙0	−12°	𝜌^𝜓0	−8°	𝜌^𝜃0	−10°
𝜌^𝜙∞	−0.3°	𝜌^𝜓∞	−0.2°	𝜌^𝜃∞	−0.2°
𝑙𝜙	0.7	𝑙𝜓	0.7	𝑙𝜃	0.7
𝛿𝜙	0.6	𝛿𝜓	0.5	𝛿𝜃	0.6
𝛿𝜙	1	𝛿𝜓	1	𝛿𝜃	1