TY - GEN
T1 - Dynamic Decoupling Control of Propeller-Engine Coupling System Based on Disturbance Observer and Feedforward-Feedback
AU - Sun, He
AU - Suo, Tao
AU - Liu, Chuanchao
AU - Zhao, Changxia
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - Aiming at the problems of propeller speed response lag, fluctuation, and thrust accuracy reduction caused by the strong bidirectional dynamic coupling effect introduced by the dynamic change of engine power, this paper deeply analyzes the essential impact, establishes an accurate propeller-engine coupling model, and innovatively proposes a feedforward-feedback composite control architecture based on a disturbance observer. The disturbance observer estimates and compensates for disturbances in real-time; the feedforward control quickly responds to commands and known disturbances; the feedback control eliminates steady-state errors and suppresses unknown disturbances. Meanwhile, a dynamic decoupling compensation strategy is introduced to effectively weaken the coupling between engine power and propeller pitch angle, and a multi-objective optimization control strategy is combined to balance various performance indicators. The specially designed decoupling controller, verified by simulation, can significantly suppress the coupling effect and improve the system's control performance (response speed, accuracy, stability) under full working conditions, proving the effectiveness and superiority of the method.
AB - Aiming at the problems of propeller speed response lag, fluctuation, and thrust accuracy reduction caused by the strong bidirectional dynamic coupling effect introduced by the dynamic change of engine power, this paper deeply analyzes the essential impact, establishes an accurate propeller-engine coupling model, and innovatively proposes a feedforward-feedback composite control architecture based on a disturbance observer. The disturbance observer estimates and compensates for disturbances in real-time; the feedforward control quickly responds to commands and known disturbances; the feedback control eliminates steady-state errors and suppresses unknown disturbances. Meanwhile, a dynamic decoupling compensation strategy is introduced to effectively weaken the coupling between engine power and propeller pitch angle, and a multi-objective optimization control strategy is combined to balance various performance indicators. The specially designed decoupling controller, verified by simulation, can significantly suppress the coupling effect and improve the system's control performance (response speed, accuracy, stability) under full working conditions, proving the effectiveness and superiority of the method.
KW - Decoupling control
KW - Feedforward control
KW - Propeller-engine coupling
KW - Variable-pitch propeller
UR - https://www.scopus.com/pages/publications/105035836253
U2 - 10.1109/AAAC66612.2025.11427490
DO - 10.1109/AAAC66612.2025.11427490
M3 - 会议稿件
AN - SCOPUS:105035836253
T3 - 2025 3rd Asian Aerospace and Astronautics Conference, AAAC 2025
SP - 190
EP - 199
BT - 2025 3rd Asian Aerospace and Astronautics Conference, AAAC 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2025 3rd Asian Aerospace and Astronautics Conference, AAAC 2025
Y2 - 26 September 2025 through 28 September 2025
ER -