Open AccessFlight Control Simulation and Flight Test of Foldable Rotor UAV
Author(s) -
Jiulong Xu,
Yongping Hao,
Shoutai Wang
Publication year - 2022
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/2252/1/012052
Subject(s) - flight test , matlab , rotor (electric) , cascade , pid controller , flight simulator , engineering , software , control theory (sociology) , flight dynamics , simulation , computer science , control (management) , control engineering , aerospace engineering , aerodynamics , mechanical engineering , artificial intelligence , temperature control , chemical engineering , programming language , operating system
Aiming at the short endurance time of micro-rotor UAV, based on the analysis of the structural characteristics and the working principle of rotor UAV, a design scheme of foldable quad-rotor UAV based on c is proposed. The feasibility of cascade PID control method is verified by co-simulation and analysis with ADAMS dynamics simulation software and MATLAB. Through the comparison of the flight test results, the feasibility of the designed control algorithm for the attitude control of the foldable quadrotor UAV is verified. Flight test shows that the UAV can achieve foldable function on the basis of stable hovering and high flight, achieved good results.