A. A. Petinrin

PID Control Design of Sideslip Angle for a Fixed-Wing Mini-UAV

B. K. Aliyu, A. A. Petinrin & J. A. Adewumi · Advances in Research · 2015

Sideslip angle is one of the state variables in the lateral state-space dynamics of an Unmanned Aerial Vehicle (UAV). Large asymmetric aerodynamic loads can be induced on a UAV’s fuselage, even at zero sideslip. For steady and level flight, this angle must be controlled. To contr...