TY - GEN
T1 - Wireless Charging System for UAV Based on High Offset Tolerance Based on Horizontal Flux Complementarity
AU - Guo, Jihua
AU - Li, Guangyao
AU - Zhu, Chunbo
N1 - Publisher Copyright:
© 2026 IEEE.
PY - 2026
Y1 - 2026
N2 - This paper presents a design scheme of unmanned aerial vehicle (UAV) wireless charging system with high lateral anti-offset tolerance, effectively solving the problem of output voltage fluctuation caused by landing position offset. The proposed coupling mechanism consists of a transmitting end and two lightweight receiving ends. The transmitting end is composed of two annular coils with a certain interval connected in reverse series, which can form a sinusoidal regularly distributed horizontal magnetic flux above the landing platform. The receiving end adopts a vertically wound solenoid structure and is installed on the left and right landing gears of the unmanned aerial vehicle. Under horizontal offset conditions, the magnetic fluxes captured by the dual receiving ends show complementary changes, which can suppress the fluctuations of the total magnetic flux and thus maintain the stability of the system output voltage. The number of turns and spacing at the transmitting end were optimized by using finite element software, which significantly reduced the mutual inductance fluctuation and expanded the allowable offset range. Based on the proposed scheme, a 300-watt experimental prototype was built. The test results show that the system can still maintain stable output under the condition of $\mathbf{\pm} \mathbf{1 0 0 m m}$ horizontal offset, with a mutual inductance fluctuation rate of approximately 8 % and a DC-DC efficiency of up to 86 %, verifying the effectiveness and practicability of the scheme.
AB - This paper presents a design scheme of unmanned aerial vehicle (UAV) wireless charging system with high lateral anti-offset tolerance, effectively solving the problem of output voltage fluctuation caused by landing position offset. The proposed coupling mechanism consists of a transmitting end and two lightweight receiving ends. The transmitting end is composed of two annular coils with a certain interval connected in reverse series, which can form a sinusoidal regularly distributed horizontal magnetic flux above the landing platform. The receiving end adopts a vertically wound solenoid structure and is installed on the left and right landing gears of the unmanned aerial vehicle. Under horizontal offset conditions, the magnetic fluxes captured by the dual receiving ends show complementary changes, which can suppress the fluctuations of the total magnetic flux and thus maintain the stability of the system output voltage. The number of turns and spacing at the transmitting end were optimized by using finite element software, which significantly reduced the mutual inductance fluctuation and expanded the allowable offset range. Based on the proposed scheme, a 300-watt experimental prototype was built. The test results show that the system can still maintain stable output under the condition of $\mathbf{\pm} \mathbf{1 0 0 m m}$ horizontal offset, with a mutual inductance fluctuation rate of approximately 8 % and a DC-DC efficiency of up to 86 %, verifying the effectiveness and practicability of the scheme.
KW - Coupler design
KW - Magnetic field simulation
KW - Misalignment tolerance
KW - UAV wireless charging
UR - https://www.scopus.com/pages/publications/105041478706
U2 - 10.1109/SECE68717.2026.11518982
DO - 10.1109/SECE68717.2026.11518982
M3 - 会议稿件
AN - SCOPUS:105041478706
T3 - 2026 2nd International Conference on Smart Energy and Control Engineering, SECE 2026
SP - 194
EP - 198
BT - 2026 2nd International Conference on Smart Energy and Control Engineering, SECE 2026
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2nd International Conference on Smart Energy and Control Engineering, SECE 2026
Y2 - 10 April 2026 through 12 April 2026
ER -