DESIGN BACKSTEPPING CONTROLLER STABILIZED PITCH ANGLE FOR FLAT-WING UAV
Keywords:
Backstepping control, Unmanned Aerial Vehicle (UAV), pitch.
Abstract
Pitch angle stability plays a very important role in stabilizing the flight path
and flight altitude of flat-wing UAVs. The article presents the results of building a
Backstepping controller to stabilize the pitching angle of a UAV. Simulation test
results on Matlab-Simulink software show that this controller ensures accuracy;
Helps stabilize the height channel even when there is strong interference.
điểm /
đánh giá
Published
2024-06-03
Issue
Section
RESEARCH AND DEVELOPMENT