TY - JOUR
T1 - Spatial trajectory tracking control for unmanned airships based on active disturbance rejection control
AU - Lou, Wenjie
AU - Zhu, Ming
AU - Guo, Xiao
N1 - Publisher Copyright:
© IMechE 2018.
PY - 2019/5/1
Y1 - 2019/5/1
N2 - In this paper, to address the spatial trajectory tracking problem of unmanned airships, a robust controller based on active disturbance rejection control is presented. By transforming the airship model to a standardized form, a straightforward design approach is adopted for the design of the controller. Active disturbance rejection control is composed of a tracking differentiator, an extended state observer, and a nonlinear state error feedback. The proposed controller replaces the conventional tracking differentiator with a third-order differentiator. The new tracking differentiator provides higher tracking precision and smoother transient process. The external disturbances and model uncertainties are observed by the extended state observer and compensated in the controller design, subsequently. Comparisons with technologies frequently used in the trajectory tracking are made through numerical simulation. The comparisons validate that the proposed controller provides satisfying performance and robustness in the presence of model uncertainty and external disturbance.
AB - In this paper, to address the spatial trajectory tracking problem of unmanned airships, a robust controller based on active disturbance rejection control is presented. By transforming the airship model to a standardized form, a straightforward design approach is adopted for the design of the controller. Active disturbance rejection control is composed of a tracking differentiator, an extended state observer, and a nonlinear state error feedback. The proposed controller replaces the conventional tracking differentiator with a third-order differentiator. The new tracking differentiator provides higher tracking precision and smoother transient process. The external disturbances and model uncertainties are observed by the extended state observer and compensated in the controller design, subsequently. Comparisons with technologies frequently used in the trajectory tracking are made through numerical simulation. The comparisons validate that the proposed controller provides satisfying performance and robustness in the presence of model uncertainty and external disturbance.
KW - Trajectory tracking
KW - active disturbance rejection control
KW - robustness
KW - tracking differentiator
KW - unmanned airship
UR - https://www.scopus.com/pages/publications/85047418821
U2 - 10.1177/0954410018774124
DO - 10.1177/0954410018774124
M3 - 文章
AN - SCOPUS:85047418821
SN - 0954-4100
VL - 233
SP - 2231
EP - 2240
JO - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
JF - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
IS - 6
ER -