With the problem of wing rock caused by asymmetric vortices, concurrent learning laws for a neural network will not converge to optimal values.[^1] For the problem of a wing-rock adaptive controller, the control matrix B is known, but the wing-rock rolling coefficient is unknown. [^1]
The destabilizing wing-rock moment is.[^1]
Where
$$\Delta=3\phi+6p$$
- rodriguezConcurrentLearningBoost[^1]
Backlinks
[[Model Reference Adaptive Control]]
State-Space Model
Wing Rock in Fighter Aircraft