TY - GEN
T1 - Active Disturbance Rejection Control Design for Compound-Wing UAV with Rotor Disturbance
AU - Hu, Yunlong
AU - Yu, Peiyuan
AU - Teng, Bochen
AU - Song, Jia
N1 - Publisher Copyright:
© 2023, Beijing HIWING Sci. and Tech. Info Inst.
PY - 2023
Y1 - 2023
N2 - Because of its vertical take-off and landing and high-speed cruise functions, compound-wing unmanned aerial vehicle (UAV) has broad application prospects in the industry. Due to its special structural design, the level flight process of compound-wing UAV will be interfered by the rotor, resulting in the decline of its control performance, which will seriously affect the flight stability of compound-wing UAV. However, it still lacks relevant research on anti-rotor disturbance. This paper presents a controller that can effectively reduce the influence of disturbances on the attitude of a compound-wing UAV. First, the compound-wing UAV model and rotor disturbance model are established. Then, the design of the active disturbance rejection control (ADRC) is carried out. Finally, the attitude control effects of PID and ADRC when the UAV is disturbed by the rotor are compared and analyzed. The simulation results show that in the case of disturbance, the ADRC has better control performance compared with PID.
AB - Because of its vertical take-off and landing and high-speed cruise functions, compound-wing unmanned aerial vehicle (UAV) has broad application prospects in the industry. Due to its special structural design, the level flight process of compound-wing UAV will be interfered by the rotor, resulting in the decline of its control performance, which will seriously affect the flight stability of compound-wing UAV. However, it still lacks relevant research on anti-rotor disturbance. This paper presents a controller that can effectively reduce the influence of disturbances on the attitude of a compound-wing UAV. First, the compound-wing UAV model and rotor disturbance model are established. Then, the design of the active disturbance rejection control (ADRC) is carried out. Finally, the attitude control effects of PID and ADRC when the UAV is disturbed by the rotor are compared and analyzed. The simulation results show that in the case of disturbance, the ADRC has better control performance compared with PID.
KW - Active disturbance rejection control
KW - Compound-wing UAV
KW - Control performance
KW - Rotor disturbance
UR - https://www.scopus.com/pages/publications/85151056688
U2 - 10.1007/978-981-99-0479-2_159
DO - 10.1007/978-981-99-0479-2_159
M3 - 会议稿件
AN - SCOPUS:85151056688
SN - 9789819904785
T3 - Lecture Notes in Electrical Engineering
SP - 1716
EP - 1723
BT - Proceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022
A2 - Fu, Wenxing
A2 - Gu, Mancang
A2 - Niu, Yifeng
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Autonomous Unmanned Systems, ICAUS 2022
Y2 - 23 September 2022 through 25 September 2022
ER -