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Figure 1.
The variation of mutual inductance within the range of square coils and rectangular coils with coil offset.
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Figure 2.
Variation in the positions of the receiving coil.
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Figure 3.
(a) Overall structure of the couplers. (b) Dimensions of each part of the couplers. (c) System architecture diagram of the UAV charging system.
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Figure 4.
System circuit structure. (a) Overall circuit diagram; (b) equivalent circuit diagram for State 1; (c) equivalent circuit diagram for State 2; (d) equivalent circuit diagram for State 3.
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Figure 5.
Flowchart of the state switching control strategy.
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Figure 6.
(a) Compensation for magnetic field strength. (b) Mutual inductance between coils with offset. (c) Variation of the charging efficiency with offset at different heights.
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Figure 7.
(a) Experimental prototype. (b) Continuous and static waveforms of the oscilloscope before and after the control logic was added. (c) Changes in efficiency during a full offset.
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Figure 8.
(a) Examples of the coupler reconstruction configuration for the SISO ccenario. (b) Coupler reconstruction configuration scheme in the MIMO scenario.
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Parameter Value Parameter Value Uin 20 V LT1 2,395 μH f 86 kHz LT2 771 μH CT1 1.43 nF LR 787 μH CT2 4.44 nF CR 4.35 nF R 50 Ω NT1 35 NT2 25 NR 90 Table 1.
System simulation parameters.
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Ref. ηDC-DC Coverage Misalignment tolerance Simplicity Comprehensive This paper 89.28% 83% $\star \star \star $ $\star \star $ $\star \star \star $ [10] 87.1% 50% $\star $ $\star \star \star $ $\star $ [25] 90.5% 44% $\star \star \star $ $\star \star \star $ $\star \star $ [26] 84.9% 60% $\star \star $ $\star \star \star $ $\star \star $ [27] 90.1% 67% $\star \star \star $ $\star \star \star $ $\star \star \star $ [28] 93.1% 40% $\star \star \star $ $\star \star \star $ $\star \star $ [29] 84.6% 67% $\star \star \star $ $\star $ $\star \star $ * The higher the number of ' ', the better the performance.$ \star $ Table 2.
Comparison between the coupler in this paper and existing research results.
Figures
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Tables
(2)