Multi-beam low-orbit satellite user grouping and resource allocation method
A technology of user grouping and low-orbit satellites, which is applied in the field of satellite user grouping and resource allocation, can solve the problem of few dynamic beam user grouping, achieve low average request waiting delay, improve satisfaction rate, and reduce complexity
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[0120] Step 1: According to the user's geographic location, the optimization goal R is to maximize the average information rate of the user M , using the convex optimization idea to divide users into M groups and optimize the center point and radius of each group to obtain the grouping result G of satellite s s ={g 1,s ,g 2,s ,…,g M,s };
[0121] The grouping diagram is as follows figure 2 shown.
[0122] Optimization objective R M It is calculated by the following process:
[0123] User k goes to the center ω of group m to which he belongs m,s The distance is r k,m,s , the off-axis angle between the antenna-to-user direction and the main axis of the antenna is θ k,m,s .
[0124]
[0125]
[0126] The hopping beam is a circular beam, and its radiation pattern is simplified as:
[0127]
[0128] Gt k,s is the transmit antenna gain of the antenna in the direction of user k, θ k,m,s is the off-axis angle from user k to the main axis of the beam, J 1 ( ) and ...
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