TY - JOUR
T1 - Anti-disturbance trajectory tracking of quadrotor vehicles via generalized extended state observer
AU - Shi, Di
AU - Wu, Zhong
AU - Chou, Wusheng
N1 - Publisher Copyright:
© The Author(s) 2019.
PY - 2020/7/1
Y1 - 2020/7/1
N2 - During the trajectory tracking process and low altitude flight of quadrotor, wind gust and ground effect will significantly affect the accuracy and stability of the controller. Therefore, it is vital for a quadrotor to have a robust controller against multiple disturbances. To mitigate this challenge, an active anti-disturbance control strategy based on generalized extended state observer is proposed in this article. Firstly, quadrotor dynamics is modeled as cascaded translational and rotational loops, and the characteristics of wind gust and ground effect are analyzed. Secondly, two generalized extended state observers are constructed for those loops respectively to estimate and attenuate the impact of wind gust and ground effect, and the position and attitude controller are designed based on backstepping method. Finally, real time experiments are carried out on hovering and circle trajectory tracking conditions. The results illustrate that the proposed controller has more advantages in high precision trajectory tracking and low altitude flight of quadrotor in existence of multiple disturbances.
AB - During the trajectory tracking process and low altitude flight of quadrotor, wind gust and ground effect will significantly affect the accuracy and stability of the controller. Therefore, it is vital for a quadrotor to have a robust controller against multiple disturbances. To mitigate this challenge, an active anti-disturbance control strategy based on generalized extended state observer is proposed in this article. Firstly, quadrotor dynamics is modeled as cascaded translational and rotational loops, and the characteristics of wind gust and ground effect are analyzed. Secondly, two generalized extended state observers are constructed for those loops respectively to estimate and attenuate the impact of wind gust and ground effect, and the position and attitude controller are designed based on backstepping method. Finally, real time experiments are carried out on hovering and circle trajectory tracking conditions. The results illustrate that the proposed controller has more advantages in high precision trajectory tracking and low altitude flight of quadrotor in existence of multiple disturbances.
KW - Quadrotor
KW - generalized extended state observer
KW - multiple disturbance
KW - trajectory tracking
KW - wind gust
UR - https://www.scopus.com/pages/publications/85077372284
U2 - 10.1177/1077546319892752
DO - 10.1177/1077546319892752
M3 - 文章
AN - SCOPUS:85077372284
SN - 1077-5463
VL - 26
SP - 1173
EP - 1186
JO - JVC/Journal of Vibration and Control
JF - JVC/Journal of Vibration and Control
IS - 13-14
ER -