TY - JOUR
T1 - Consensus-Based Powered Cruise and Yaw Controls for Unmanned Aerial Vehicle With Distributed Electric Propulsion System
AU - Yuan, Cong
AU - Du, Yuhua
AU - Huangfu, Yigeng
AU - Gong, Chao
AU - Gao, Fei
AU - Li, Zhipeng
N1 - Publisher Copyright:
© 2013 IEEE.
PY - 2025
Y1 - 2025
N2 - The distributed electric propulsion (DEP) system has been favored over the conventional centralized propulsion system in applications of unmanned aerial vehicles (UAVs). However, most existing techniques in propulsion system management adopt centralized control approaches, which could not fully utilize the decentralized features brought out by the DEP system. This article proposes a novel control approach for UAVs with the DEP system (DEP-UAV). The propellers in the DEP system are coordinated in a distributed manner to collectively regulate the UAV’s flight speed and course angle, which are known as powered cruise and yaw controls. To prevent the UAV from stalling out, the powered cruise and yaw controls over each propeller are designed to be sufficiently decoupled. Detailed controller designs and stability analyses are presented. The proposed distributed control algorithm has been fully implemented on hardware devices and validated on a controller hardware-in-the-loop (C-HIL) testbed for DEP-UAV. The experimental results indicate that without the decoupling between cruise and course controls, the DEP-UAV becomes unstable after 100 s and ultimately stalls. However, with the proposed control system in place, a deviation in flight speed is efficiently corrected with minimal overshoot, and the desired course angle adjustment is achieved.
AB - The distributed electric propulsion (DEP) system has been favored over the conventional centralized propulsion system in applications of unmanned aerial vehicles (UAVs). However, most existing techniques in propulsion system management adopt centralized control approaches, which could not fully utilize the decentralized features brought out by the DEP system. This article proposes a novel control approach for UAVs with the DEP system (DEP-UAV). The propellers in the DEP system are coordinated in a distributed manner to collectively regulate the UAV’s flight speed and course angle, which are known as powered cruise and yaw controls. To prevent the UAV from stalling out, the powered cruise and yaw controls over each propeller are designed to be sufficiently decoupled. Detailed controller designs and stability analyses are presented. The proposed distributed control algorithm has been fully implemented on hardware devices and validated on a controller hardware-in-the-loop (C-HIL) testbed for DEP-UAV. The experimental results indicate that without the decoupling between cruise and course controls, the DEP-UAV becomes unstable after 100 s and ultimately stalls. However, with the proposed control system in place, a deviation in flight speed is efficiently corrected with minimal overshoot, and the desired course angle adjustment is achieved.
KW - Distributed control
KW - distributed propulsion system
KW - energy efficiency
KW - finite-time consensus
KW - fixed-time consensus
KW - unmanned aerial vehicle (UAV)
UR - http://www.scopus.com/inward/record.url?scp=105003806194&partnerID=8YFLogxK
U2 - 10.1109/JESTPE.2024.3449437
DO - 10.1109/JESTPE.2024.3449437
M3 - 文章
AN - SCOPUS:105003806194
SN - 2168-6777
VL - 13
SP - 1769
EP - 1782
JO - IEEE Journal of Emerging and Selected Topics in Power Electronics
JF - IEEE Journal of Emerging and Selected Topics in Power Electronics
IS - 2
ER -