Combined optimization method used for synthesis of large-scale heterogeneous four-dimensional antenna array
A joint optimization and heterogeneous technology, applied in the direction of manufacturing antenna array devices, antenna combinations with different interactions, antenna arrays, etc., can solve the problems of slow convergence, infeasibility, low efficiency, etc., to improve speed and efficiency. , the effect of increasing speed and efficiency
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Embodiment 1
[0060] Example 1: Synthesis of low-sidelobe heterogeneous 4D arrays based on a simple aircraft model in an unscanned state
[0061] Consider a heterogeneous four-dimensional array. There are 4 heterogeneous arrays in total, which are composed of a cylindrical fuselage surface array, a nose plane array, and left and right wing plane arrays. The structure is as follows: Figure 4 shown. The number of fuselage units is 4×10×16=640. There are 20 units along the direction of the busbar and 32 units in the direction of the alignment. 4 indicates the number of sub-arrays in which the units are symmetrically distributed, that is, there are four 10×16 units on the fuselage. The sub-arrays are composed of sub-arrays, and the equivalent excitation amplitude (switch closing duration) of the sub-arrays is the same, the number of nose units is 4×16×16=1024, the number of right wing units is 4×10×10=400, and the The number of wing units is 4×10×10=400, and they are all symmetrically distrib...
Embodiment 2
[0064] Embodiment 2: under the scanning state based on simple aircraft model (θ 0 =45. , ) low sidelobe heterogeneous 4D array synthesis
[0065] In this case, the number of heterogeneous arrays is considered to be 3 in total, which are composed of a cylindrical fuselage surface array, a nose plane array, and a right wing plane array. constant. The number of fuselage units is 4×10×10=400. There are 20 units along the direction of the busbar and 20 units in the direction of the directrix. 4 indicates the number of sub-arrays with symmetrical distribution of units, that is, there are four 10×10 units on the fuselage. The sub-arrays are composed, and the equivalent excitation amplitude (switch closing duration) of the units between sub-arrays is the same, the number of nose units is 4×14×14=784, the number of right wing units is 4×10×10=400, and They are all similar to the symmetrical distribution of the fuselage. The switching sequence adopts pulse phase shift, and the stat...
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