In order to research the ability of the UAV to correct deviation during the front three-wheel taxiing phase and establish accurate taxi model of the drone, this paper takes a certain UAV with nose-wheel landing gear as the research object. This paper conducts a complete dynamic analysis of its ground model, improves the ground force analysis and aerodynamic analysis, builds a 6-demention model which contains a PID controller and adds a LADRC controller in Matlab for verifying the anti-disturbance ability of LADRC of the UAV in the model. The result shows that compared with PID controller, LADRC can effectively suppress heading deviation caused by the disturbance, and the drone can be more quickly aligned to the heading for the UAV rolling under disturbance.
UAV Taxiing Control Based on Linear Active Disturbance Rejection Control
2021-06-01
1310078 byte
Conference paper
Electronic Resource
English
Event-Triggered Active Disturbance Rejection Control
Springer Verlag | 2021
|Linear active disturbance rejection control of the hovercraft vessel model
BASE | 2015
|Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection
DOAJ | 2022
|