TY - GEN
T1 - Disturbance Observer-based Control of Quadrotors with Motor Response Delay and Throttle Nonlinearity
AU - Song, Yansui
AU - Liu, Xi
AU - Xu, Bin
AU - Zhang, Yu
AU - Yang, Chenguang
N1 - Publisher Copyright:
© 2020 IEEE.
PY - 2020/9
Y1 - 2020/9
N2 - This paper proposes a nonlinear disturbance observer-based controler (NDOBC) for quadrotors considering the motor response delay and the throttle nonlinear. A simplified quadrotor dynamic model which includes the attitude model and propulsion system is used to design the nonlinear disturbance observer. The NDOBC is sensitive to the motor response delay, which is founded by the experiment. Furthermore, if this is not handled appropriately, the system might go unstable. An equivalent motor response delay module is inserted between the observer and the controller output. To eliminate the influence of the throttle nonlinearity, a method is given by solving quadratic functions about the pseudo throttle. The simulation results show that the proposed method can guarantee the system stability and get a well noise suppression capability. In addition, a higher attitude control accuracy is achieved by eliminating the throttle nonlinearity.
AB - This paper proposes a nonlinear disturbance observer-based controler (NDOBC) for quadrotors considering the motor response delay and the throttle nonlinear. A simplified quadrotor dynamic model which includes the attitude model and propulsion system is used to design the nonlinear disturbance observer. The NDOBC is sensitive to the motor response delay, which is founded by the experiment. Furthermore, if this is not handled appropriately, the system might go unstable. An equivalent motor response delay module is inserted between the observer and the controller output. To eliminate the influence of the throttle nonlinearity, a method is given by solving quadratic functions about the pseudo throttle. The simulation results show that the proposed method can guarantee the system stability and get a well noise suppression capability. In addition, a higher attitude control accuracy is achieved by eliminating the throttle nonlinearity.
UR - http://www.scopus.com/inward/record.url?scp=85094964708&partnerID=8YFLogxK
U2 - 10.1109/ICUAS48674.2020.9213843
DO - 10.1109/ICUAS48674.2020.9213843
M3 - 会议稿件
AN - SCOPUS:85094964708
T3 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
SP - 182
EP - 187
BT - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
Y2 - 1 September 2020 through 4 September 2020
ER -