DESIGN BACKSTEPPING CONTROLLER STABILIZED PITCH ANGLE FOR FLAT-WING UAV

  • Đặng Tiến Trung
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
Section
RESEARCH AND DEVELOPMENT