Low-orbit/middle-orbit double-layer satellite optical network structure system and design calculation method
A network structure and low-orbit satellite technology, applied in the field of satellite network structure, can solve problems such as large network delay and no consideration of inter-satellite laser link characteristics, and achieve the effects of reducing handover, strengthening implementation management, and simplifying network routing
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Embodiment 1
[0117] Let H be the altitude of the satellite, R be the radius of the Earth, and ε be the elevation angle of the ground station to the satellite. exist Figure 8 In the schematic diagram of the coverage zone shown, two satellites form a coverage zone, θ is the radius of a single satellite coverage circle, and its value is:
[0118] ①, θ=arccos[Rcosε / (R+H)]-ε
[0119] Ψ is the half-angle of the coverage zone, and 2π / S is the distance between two satellites in the orbital plane, which is known from the spherical right triangle theorem:
[0120] ②、Ψ=arccos[cosθ / cos(π / S)]
[0121] The satellite positions of the orbit B closest to the reference satellite (ahead of satellite A) are:
[0122] ③,
[0123] The constraints to satisfy continuous coverage are:
[0124] ④, α′≤Ψ+arccos[cosθ / cosδ B ]
[0125] Using the spherical right triangle theorem, we know that the actual right ascension difference:
[0126] ⑤、sinα=sinα′ / sini
[0127] The relationship between the actual phase ...
Embodiment 2
[0135] Let H be the altitude of the satellite, R be the radius of the Earth, and ε be the elevation angle of the ground station to the satellite. exist Figure 8 In the schematic diagram of the coverage zone shown, two satellites form a coverage zone, θ is the radius of a single satellite coverage circle, and its value is:
[0136] ①, θ=arccos[Rcosε / (R+H)]-ε
[0137] Ψ is the half-angle of the coverage zone, and 2π / S is the distance between two satellites in the orbital plane, which is known from the spherical right triangle theorem:
[0138] ②、Ψ=arccos[cosθ / cos(π / S)]
[0139] The satellite positions of the orbit B closest to the reference satellite (ahead of satellite A) are:
[0140] ③,
[0141] The constraints to satisfy continuous coverage are:
[0142] ④, α′≤Ψ+arccos[cosθ / cosδ B ]
[0143] Using the spherical right triangle theorem, we know that the actual right ascension difference:
[0144] ⑤、sinα=sinα′ / sini
[0145] The relationship between the actual phase ...
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