Spatial domain non-uniform pilot design method
A pilot design and non-uniform technology, applied in the field of communication, can solve problems affecting the quality of CSI estimation
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Embodiment 1
[0045] The embodiment of the present invention proposes a method for designing non-uniform pilots in the space domain, see figure 1 , the method includes the following steps: Knowing the total number of transmitting antennas N t and the number of antennas N used to transmit the pilot p ;
[0046] Step 101: According to the autocorrelation matrix of the antennas in the transmitting antenna array, based on the criterion of satisfying the signal independence and maximizing the sparse characteristics, select the channel sparse matrix from the transmitting antenna to the receiving antenna
[0047] Step 102: If the energy distribution of the pilot symbols on the pilot antenna is given, based on the criterion of minimizing the correlation between the channel sparse base matrix Ψ and the pilot symbol matrix X, a pilot symbol insertion model is obtained, where the pilot symbol matrix is the pilot symbol sequence;
[0048] If the pilot symbol insertion model is given, based on ...
Embodiment 2
[0052] In this embodiment of the present invention, taking the energy distribution of known pilot symbols as an example, the specific implementation process of the airspace non-uniform pilot design method of the present invention is introduced in detail, see figure 2 , including the following steps: Knowing the total number of transmitting antennas N t and the number of antennas N used to transmit the pilot p ;
[0053] Step 201: Calculate the antenna autocorrelation matrix R t .
[0054] In this step, the antenna autocorrelation matrix in the antenna array Let the autocorrelation matrix between horizontal and vertical antennas be R x and R y ,Have , since the antenna spacing of the two-dimensional large-scale antenna array is less than one wavelength, there is a certain correlation between the channels from different antennas to the receiving antenna, and the correlation can be expressed by N t ×N t Dimensional autocorrelation coefficient matrix, the (i, j) element...
Embodiment 3
[0082] In this embodiment of the present invention, the known pilot symbol insertion model is taken as an example to introduce in detail the specific implementation process of the airspace non-uniform pilot design method of the present invention, see Figure 6 , including the following steps: Knowing the total number of transmitting antennas N t and the number of antennas N used to transmit the pilot p ;
[0083] Step 601: Calculate the antenna autocorrelation matrix R t .
[0084] In this step, the antenna autocorrelation matrix in the antenna array Let the autocorrelation matrix between horizontal and vertical antennas be R x and R y ,Have
[0085] Step 602: Select a channel sparse base matrix according to the antenna autocorrelation matrix.
[0086] In this step, assuming that the receiving antenna of each user is a single antenna, the channel from the base station to each user Modeling has: h=(R t ) 1 / 2 h iid ,in It is a vector that represents the random...
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