TY - GEN
T1 - A Multi-Motor Consensus Control Against Disturbances for Cruise of DEP UAV
AU - Qu, Tao
AU - Kong, Honghua
AU - Sun, Tianjian
AU - Liang, Zihao
AU - Zhang, Ruiheng
AU - Quan, Sheng
AU - Du, Yuhua
AU - Fan, Aili
AU - Huangfu, Yigeng
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - For unmanned aerial vehicle (UAV) with a distributed electric propulsion system (DEP), external disturbances may disrupt the synchronization among the motors at each thruster, leading to unbalanced moments during cruise. This paper proposes a novel multi-motor consensus control method for the DEP system. The key innovation lies in an error constraint strategy that rigorously confines the motor's rotation speed errors within prescribed bounds, ensuring coordinated motor operation while simultaneously enabling precise flight speed adjustment. In addition, the controller operates without requiring system parameter identification or disturbance measurements, and relies solely on the feedback rotation speed of the motors. Stability guarantees are analytically established via Lyapunovbased proofs, while comparative numerical simulations validate the method's superiority in disturbance rejection.
AB - For unmanned aerial vehicle (UAV) with a distributed electric propulsion system (DEP), external disturbances may disrupt the synchronization among the motors at each thruster, leading to unbalanced moments during cruise. This paper proposes a novel multi-motor consensus control method for the DEP system. The key innovation lies in an error constraint strategy that rigorously confines the motor's rotation speed errors within prescribed bounds, ensuring coordinated motor operation while simultaneously enabling precise flight speed adjustment. In addition, the controller operates without requiring system parameter identification or disturbance measurements, and relies solely on the feedback rotation speed of the motors. Stability guarantees are analytically established via Lyapunovbased proofs, while comparative numerical simulations validate the method's superiority in disturbance rejection.
KW - DEP UAV
KW - disturbance injection capability
KW - moment balance
KW - multi-motor consensus control
UR - https://www.scopus.com/pages/publications/105011034198
U2 - 10.1109/IAS62731.2025.11061598
DO - 10.1109/IAS62731.2025.11061598
M3 - 会议稿件
AN - SCOPUS:105011034198
T3 - Conference Record - IAS Annual Meeting (IEEE Industry Applications Society)
BT - 2025 IEEE Industry Applications Society Annual Meeting, IAS 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2025 IEEE Industry Applications Society Annual Meeting, IAS 2025
Y2 - 15 June 2025 through 20 June 2025
ER -