TY - JOUR
T1 - A New Disturbance Attenuation Control Scheme for Quadrotor Unmanned Aerial Vehicles
AU - Xiao, Bing
AU - Yin, Shen
N1 - Publisher Copyright:
© 2005-2012 IEEE.
PY - 2017/12
Y1 - 2017/12
N2 - This paper addresses a difficult problem of high-accuracy control for quadrotor unmanned aerial vehicles (UAVs) subject to external disturbance force and unknown disturbance torque. An observer-based full control scheme is presented. In the strategy, two observer-based estimators are first designed to estimate external disturbance force and torque, respectively. With the application of the precise estimation value, a nonlinear tracking controller is then proposed with compensated disturbance. It is shown by the Lyapunov stability analysis that the entire controller-observer system is asymptotically stable. The key feature of the scheme is that it not only has the superior capability to attenuate unknown external disturbance torque and external force generated by the wind, but also it is able to achieve full control (i.e., six degrees-of-freedom) of the quadrotor UAVs with position and attitude successfully controlled. The effectiveness of the approach is verified on a quadrotor UAV example.
AB - This paper addresses a difficult problem of high-accuracy control for quadrotor unmanned aerial vehicles (UAVs) subject to external disturbance force and unknown disturbance torque. An observer-based full control scheme is presented. In the strategy, two observer-based estimators are first designed to estimate external disturbance force and torque, respectively. With the application of the precise estimation value, a nonlinear tracking controller is then proposed with compensated disturbance. It is shown by the Lyapunov stability analysis that the entire controller-observer system is asymptotically stable. The key feature of the scheme is that it not only has the superior capability to attenuate unknown external disturbance torque and external force generated by the wind, but also it is able to achieve full control (i.e., six degrees-of-freedom) of the quadrotor UAVs with position and attitude successfully controlled. The effectiveness of the approach is verified on a quadrotor UAV example.
KW - Asymptotic stability
KW - disturbance attenuation
KW - estimator
KW - quadrotor unmanned aerial vehicle (UAV)
KW - tracking control
UR - http://www.scopus.com/inward/record.url?scp=85021406167&partnerID=8YFLogxK
U2 - 10.1109/TII.2017.2682900
DO - 10.1109/TII.2017.2682900
M3 - 文章
AN - SCOPUS:85021406167
SN - 1551-3203
VL - 13
SP - 2922
EP - 2932
JO - IEEE Transactions on Industrial Informatics
JF - IEEE Transactions on Industrial Informatics
IS - 6
M1 - 7879324
ER -