Title : 
Quadrotor unmanned helicopter attitude control based on improved ADRC
         
        
            Author : 
Guo-Yan Xia ; Zheng-Hua Liu
         
        
            Author_Institution : 
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
         
        
        
        
        
        
            Abstract : 
A kind of attitude control method for the quadrotor unmanned helicopter based on improved active disturbance rejection control (ADRC) is proposed in this paper. The dynamic model of the quadrotor unmanned helicopter is built, and the virtual control is introduced, then the non-linear model is decomposed into height, yaw, roll and pitch of the four independent channels and the disturbance rejection control technology is applied into the various channels. The simulation results show that ADRC can achieve the attitude augmentation control of the helicopter and have a good robustness. Also the results show that the improved ADRC is superior to classical ADRC both on performance and adaptability.
         
        
            Keywords : 
active disturbance rejection control; aircraft control; attitude control; helicopters; nonlinear control systems; ADRC; active disturbance rejection control; attitude augmentation control; attitude control method; disturbance rejection control technology; dynamic model; nonlinear model; quadrotor unmanned helicopter attitude control; virtual control; Attitude control; Educational institutions; Force; Helicopters; Mathematical model; Robustness; Rotors; attitude control; improved ADRC; quadrotor unmanned helicopter; robustness;
         
        
        
        
            Conference_Titel : 
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
         
        
            Conference_Location : 
Yantai
         
        
            Print_ISBN : 
978-1-4799-4700-3
         
        
        
            DOI : 
10.1109/CGNCC.2014.7007331