Traditional control systems like Nonlinear Dynamic Inversion (NDI) rely heavily on precise mathematical models. While this worked well for conventional aircraft, it falls short in today’s complex, ...

There was a significant difference in perceived instability (p = 0.01, CAI group = 4.14 ± 2.48 cm, control group = 0.99 ± 1.3 cm). Conclusions These results indicate that despite the similarities ...