TY - GEN
T1 - Sigmiod based anti-disturbances trajectory tracking for quadrotor UAV under gyroscope noise
AU - Kou, Zhan
AU - Wang, Honglun
AU - Su, Zikang
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - In this paper, a Sigmiod based anti-disturbances trajectory tracking controller is developed to cope with the trajectory tracking problem of the quadrotor under external disturbances, model uncertainties and gyroscope noise. Firstly, the accurate nonlinear dynamic model of quadrotor UAV is established. Then, based on the hierarchical control principle, the trajectory tracking controller is designed as position loop and attitude loop respectively, each loop constructs the corresponding controller by feedback linearization. In addition, the high-order sigmoid tracking differentiator (STD) is developed to generate the required differential signal and arrange expected transition process, synchronously, the sigmoid disturbance observer (SDO) with the same frame as the STD is applied to reconstruct the lump disturbances of the attitude loop and the position loop. At last, the simulation results demonstrate that the proposed controller not only ensures small tracking error and strong noise suppression, but also simplifies the structure of controller and make it easy to adjust controller parameters.
AB - In this paper, a Sigmiod based anti-disturbances trajectory tracking controller is developed to cope with the trajectory tracking problem of the quadrotor under external disturbances, model uncertainties and gyroscope noise. Firstly, the accurate nonlinear dynamic model of quadrotor UAV is established. Then, based on the hierarchical control principle, the trajectory tracking controller is designed as position loop and attitude loop respectively, each loop constructs the corresponding controller by feedback linearization. In addition, the high-order sigmoid tracking differentiator (STD) is developed to generate the required differential signal and arrange expected transition process, synchronously, the sigmoid disturbance observer (SDO) with the same frame as the STD is applied to reconstruct the lump disturbances of the attitude loop and the position loop. At last, the simulation results demonstrate that the proposed controller not only ensures small tracking error and strong noise suppression, but also simplifies the structure of controller and make it easy to adjust controller parameters.
UR - https://www.scopus.com/pages/publications/85082484091
U2 - 10.1109/GNCC42960.2018.9019034
DO - 10.1109/GNCC42960.2018.9019034
M3 - 会议稿件
AN - SCOPUS:85082484091
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -