Fig. 5
Attitude tracking performance (roll \(\phi\), pitch \(\theta\), yaw \(\psi\)) of the quadrotor UAV under nominal conditions using MPSO-RBF FTC.
Fig. 5 | Scientific Reports
Attitude tracking performance (roll \(\phi\), pitch \(\theta\), yaw \(\psi\)) of the quadrotor UAV under nominal conditions using MPSO-RBF FTC.
