Method for generating multiple orbital angular momentum beams
A technology of orbital angular momentum and multi-beam, which is applied to antennas, electrical components, and radiation element structures, can solve the problems of small coverage, complex structure, and single mode, and achieve low cost, high radiation efficiency, and low loss. Effect
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Embodiment 1
[0041] Embodiment 1: Generate orbital angular momentum vortex beams with radiation mode numbers of 1 in different directions.
[0042] Step 1, select the geometric positional relationship.
[0043] 1a) Set parameters:
[0044] refer to figure 2 , take the relative position of the center of horn 1 antenna m, that is, 0 on the x-axis, 0 on the y-axis, and 0.4 meters on the z-axis; two angular momentum beams are set to be generated, and the radiation direction of the first angular momentum beam is set as The radiation direction of the second angular momentum beam is set as The total number of rows M=20 of the electromagnetic metasurface reflection unit, the total number of columns N=20, the distance between the centers of two adjacent electromagnetic metasurface reflection units D=25 millimeters, the size of the dielectric substrate 22 is 0.5 × 0.5 × 0.001 meters, the electromagnetic metasurface The size of the surface reflection unit 21 is 25×25 mm; the distance d betw...
Embodiment 2
[0062] Embodiment 2: Generate orbital angular momentum vortex beams with 2 radiation modes in different directions.
[0063] Step 1, select the geometric positional relationship.
[0064] Referring to Embodiment 1, the geometric positional relationship consistent with Embodiment 1 is selected.
[0065] Step 2, calculate the compensation phase required for each electromagnetic metasurface reflection unit
[0066] 2.1) Given that the operating frequency f of the horn antenna is 5.8GHz, take the eigenmode number l of the first angular momentum beam 1 = 2, the eigenmode number l of the second angular momentum beam 2 =2, calculate the required compensation phase of each electromagnetic metasurface reflection unit with reference to the method given in Embodiment 1
[0067] 2.2) Compensate the phase according to the calculated mth row and nth column The value of , draw the phase distribution map of all electromagnetic metasurface reflection units, such as Figure 7 as shown...
Embodiment 3
[0076] Embodiment 3: Generate orbital angular momentum vortex beams with radiation mode numbers of 1 and 2 in different directions.
[0077] Step A, select the geometric positional relationship.
[0078] Referring to Embodiment 1, the geometric positional relationship consistent with Embodiment 1 is selected.
[0079] Step B, calculate the compensation phase required for each electromagnetic metasurface reflection unit
[0080] B1) Given that the operating frequency f of the horn antenna is 5.8GHz, take the eigenmode number l of the first angular momentum beam 1 = 1, the eigenmode number l of the second angular momentum beam 2 =2, calculate the required compensation phase of each electromagnetic metasurface reflection unit with reference to the method given in Embodiment 1
[0081] B2) Compensate the phase according to the calculated mth row and nth column The value of , draw the phase distribution map of all electromagnetic metasurface reflection units, such as Fig...
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