TY - GEN
T1 - The attitude control of UAV in carrier landing based on ADRC
AU - Yu, Yue
AU - Wang, Honglun
AU - Shao, Xingling
AU - Huang, Yu
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC) to solve the problem. Firstly, UAV model including windy and windless condition and disturbance model are introduced. Next, ADRC-based controller is designed for UAV model. Finally, a series of numerical simulations are presented. The simulation results demonstrate that ADRC has an excellent performance in terms of estimation of states and internal and external disturbance, attitude tracking, disturbance rejection and robustness to model uncertainties.
AB - In this paper, the problem of unmanned aerial vehicle(UAV) pitch angle control is considered. We employ a method of active disturbance rejection control(ADRC) to solve the problem. Firstly, UAV model including windy and windless condition and disturbance model are introduced. Next, ADRC-based controller is designed for UAV model. Finally, a series of numerical simulations are presented. The simulation results demonstrate that ADRC has an excellent performance in terms of estimation of states and internal and external disturbance, attitude tracking, disturbance rejection and robustness to model uncertainties.
UR - https://www.scopus.com/pages/publications/85015210706
U2 - 10.1109/CGNCC.2016.7828893
DO - 10.1109/CGNCC.2016.7828893
M3 - 会议稿件
AN - SCOPUS:85015210706
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 832
EP - 837
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -