Transmit method based on satellite massive MIMO integrated sensing and communication

Abstract

Disclosed is a transmit method based on satellite massive Multiple-Input Multiple-Output (MIMO) integrated sensing and communication, where a satellite end is equipped with a massive MIMO array to implement an integrated sensing and communication system. The satellite end sends a communication signal to multiple user terminals based on statistical properties of electromagnetic wave propagation, and detects multiple targets simultaneously, thus realizing simultaneous communication of the satellite end with the user terminals and sensing for the targets. The present disclosure fully utilizes the spectrum resources, implements a flexible switch between wireless communication and target sensing functions based on a satellite, and mitigates the effects of the beam squint on system performance, thus greatly improving communication performance and radar resolution and being applicable for construction of an integrated network of space, air, ground and sea to achieve global coverage.

Description

TECHNICAL FIELD

The present disclosure relates to a transmit method based on satellite massive Multiple-Input Multiple-Output (MIMO) integrated sensing and communication.

BACKGROUND

With the rapid development of wireless industry, spectrum resources become increasingly scarce and the value thereof becomes increasingly high. In order to improve the utilization of the spectrum resources, an integrated sensing and communication method and system are proposed to achieve frequency reuse between two functional modules of wireless communication and radar sensing. In the integrated sensing and communication system, communication and sensing can be simultaneously conducted on the same hardware platform, to make decongestion of an RF environment possible. The existing integrated sensing and communication work is mainly focused on the terrestrial network, and many designs have been explored, so as to improve the performance of the two functional modules.

For a satellite massive MIMO integrated sensing and communication system, its electromagnetic wave propagation characteristics are significantly different from those in the terrestrial network, and therefore, a terrestrial integrated sensing and communication system cannot be directly used. Specifically, there are mainly two aspects: First, because the distance between the satellite and the user terminal as well as the target is relatively long, a high propagation delay is caused; and further, the mobility of the user terminal and the detection target may lead to a large Doppler shift. In addition, considering that the wideband satellite massive MIMO integrated sensing and communication system employs a large number of antennas and wideband transmission, the channel dimension is large and changes rapidly, which poses a challenge to the estimation of status information of electromagnetic wave propagation. In general cases, for the satellite massive MIMO integrated sensing and communication system, at the satellite-side transmitter end, it is difficult to obtain accurate instantaneous status information of electromagnetic wave propagation.

SUMMARY

Invention Objective

For the foregoing prior art, a satellite massive MIMO integrated sensing and communication method and system based on statistical status information of electromagnetic wave propagation and taking beam squint into consideration are proposed, which can effectively mitigate the effects of the beam squint on system performance, realize efficient utilization of spectrum resources, and implement a flexible switch between wireless communication and target sensing, thus greatly improving energy efficiency of communication and radar resolution.

Technical Solution

A transmit method based on satellite massive MIMO integrated sensing and communication is provided, where a satellite end is equipped with a massive MIMO antenna array which simultaneously serves multiple users and detects multiple targets. Communication and sensing use the same spectrum resources and the same hardware platform, and integrated sensing and communication is implemented by transmitting a signal to focus on communication or sensing. The satellite end estimates statistical status information of electromagnetic wave propagation according to received uplink and downlink pilot signals, where for a communication process, the statistical status information of electromagnetic wave propagation is a channel gain and a channel direction vector between the satellite end and user terminals; and for a sensing process, the statistical status information of electromagnetic wave propagation is angles of departure of the targets. According to the statistical status information of electromagnetic wave propagation, the satellite end transmits a directional beam to a detection target and a downlink signal to each user terminal by means of integrated sensing and communication precoding. During the dynamic movement of the satellite and the user terminals as well as the targets, with the change in the statistical status information of electromagnetic wave propagation between the satellite and the user terminals as well as the targets, the integrated sensing and communication precoding is updated.

Advantageous Effects

A satellite massive MIMO integrated sensing and communication method of the present disclosure has the following advantages:

• • (1) In the present disclosure, statistical properties of electromagnetic wave propagation that considers beam squint are modelled, thus establishing a relationship between the degree of beam squint and system-related parameters.
  • (2) In the present disclosure, the transmitter of the system can execute communication and sensing functions simultaneously, and adjust the weight of the two functional modules by introducing a weighting coefficient, so as to weigh communication energy efficiency and estimation accuracy of a radar beam mode.
  • (3) In the present disclosure, a hybrid precoding method is designed, so as to mitigate the effects of the beam squint, thus enhancing the energy efficiency and performance of communication and the resolution of radar sensing.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic diagram of a satellite massive MIMO integrated sensing and communication system; and

FIG. 2 is a schematic diagram of configuration of a massive antenna array at a satellite end.

DETAILED DESCRIPTION OF THE EMBODIMENTS

The present disclosure is further explained below with reference to the accompanying drawings.

In a satellite massive MIMO integrated sensing and communication method, a satellite end is equipped with a massive MIMO antenna array which simultaneously serves multiple users and detects multiple targets, as shown in FIG. 1. Communication and sensing use the same spectrum resources and the same hardware platform, and integrated sensing and communication is implemented by transmitting a signal to focus on communication or sensing, where a communication process includes channel estimation and data transmission, and a sensing process includes target search by radar and beam forming. The satellite end estimates statistical status information of electromagnetic wave propagation according to received uplink and downlink pilot signals, where for the communication process, the statistical status information of electromagnetic wave propagation is a channel gain and a channel direction vector between the satellite end and user terminals; and for the sensing process, the statistical status information of electromagnetic wave propagation is angles of departure of the targets.

According to the statistical status information of electromagnetic wave propagation, the satellite end transmits a directional beam to a detection target and a downlink signal to each user terminal by means of integrated sensing and communication precoding, where the integrated sensing and communication precoding is a hybrid precoding scheme based on an energy efficiency maximization principle and a convex optimization algorithm. Each antenna unit of the massive MIMO antenna array sends signals independently by using a fully digital or analog or hybrid transmission manner. In the process of simultaneously implementing communication and sensing, the performance of communication and sensing is weighed by introduction of a weighting coefficient, so as to realize a flexible switch between wireless communication and target sensing functions. During the dynamic movement of the satellite and the user terminals as well as the targets, with the change in the statistical status information of electromagnetic wave propagation between the satellite and the user terminals as well as the targets, the integrated sensing and communication precoding is updated.

Specifically, as shown in FIG. 2, the satellite end is equipped with a massive MIMO antenna array which includes more than hundreds of antenna units, where each antenna unit may be a unipolar or multipolar antenna. The array structure is a uniform surface array, where the numbers of antennas in the x and y directions are N_t^x and N_t^y respectively, and then a total number of the antennas is N_t=N_t^x×N_t^y; and a spacing between the antennas is r. Further, a hybrid analog/digital transmitter is used to serve K single antenna users, and each user terminal uses a fully digital receiver. Multiple targets are detected simultaneously, and the number of RF chains required by the transmitter is M_t, where K≤M_t≤N_t.

Considering frequency selectivity of a wideband massive MIMO low earth orbit satellite system, inter-symbol interference is reduced by means of Orthogonal Frequency Division Multiplexing (OFDM). That is, M sub-carriers are used in total for a signal bandwidth B_w, and then the spacing between the sub-carriers is Δ_b=B_w/M. Thus, the frequency of the mth sub-carrier is:

$\begin{array}{cc}{f}_m=\left(m-\frac{M+1}{2}\right){\Delta }_B,m=1,2,\dots ,M.& \left(1\right)\end{array}$ 1. Communication Module(1) Modeling of Statistical Properties of Multipath Channel Propagation that Considers Beam Squint

It is noted that the satellite altitude is much higher than the scatterers around the terrestrial user terminals. If there are in total L_k propagation paths for the kth user, the propagation paths are set to have the same angle ϑ_k=(ϑ_k^x, ϑ_k^y) of departure, where ϑ_k^x and ϑ_k^y denote angles of departure in the x and y directions respectively. If a propagation delay on the lth path is τ_k,l, a total delay τ_k,l,ny,ny to the (n_x, n_y)th element in the antenna array is:τ_k,l,nx,ny=τ_k,l+_nx,ny(ϑ_k),  (2)

The second term in the equation refers to a time delay from the (l,l)th element to the (n_x, n_y)th element in the antenna array for the kth user, namely:

$\begin{array}{cc}{\tau }_{n_x,n_y}\left({\vartheta }_k\right)\stackrel{△}{=}\frac{r\left(\left(n_x-1\right){\vartheta }_k^x+\left(n_y-1\right){\vartheta }_k^y\right)}{c},& \left(3\right)\end{array}$ where n_x∈{1,2, . . . , N_t^x} and n_y∈{1,2, . . . , N_t^y} denote antenna unit numbers in the x and y directions respectively, and c denotes the velocity of light.

Assuming that a channel gain of the lth path for the kth user is a_k,l and the Doppler gain is v_k,l, a downlink channel space-frequency response h_k,nx,ny(t, f) between the kth user and the (n_x, n_y)th element of the low earth orbit satellite-end antenna array at the time t and the frequency f is:

$\begin{array}{cc}{h}_{k,n_x,n_y}\left(t,f\right)=\sum _{l=1}^{L_k}{\alpha }_{k,l}\exp \left\{\mathrm{𝒿2}\pi \left[{\mathrm{tv}}_{k,l}-f{\tau }_{k,l}\right]\right\}\exp \left\{-\mathrm{𝒿2\pi }\left(f_c+f\right){\gamma }_{n_x,n_y}\left({\vartheta }_k\right)\right\},& \left(4\right)\end{array}$ where exp {□} denotes an exponential operator, ø=√{square root over (−1)}, and f_c denotes the carrier frequency. The above equation is rearranged and vectorized to obtain the following baseband downlink channel space-frequency response vector after time-frequency synchronization:h_k(t,f)=v_k(f)g_k(t,f),  (5)where the channel gain g_k(t,f) follows the Rician distribution with a parameter being the Rician parameter κ_k and its energy meets E{|g_k(t, f)|²}=γ_k, γ_k being the channel energy between the satellite and the kth user and E{┘} denoting an operator for evaluation of expectation; and v_k(f) is an array response vector and meets the following formula:v_k(f)□v(f,ϑ_k)=v_k^x(f)⊗v_k^y(f)=v_x(f,ϑ_k^x)⊗v_y(f,ϑ_k^y)∈□^Nt×1,  (6)where □^m×n denotes a subspace with dimensions of m×n, and ⊗ denotes the Kronecker product; and in the case of d∈D□{x, y}, there is the following formula:

$\begin{array}{cc}{v}_k^d\left(f\right)\stackrel{△}{=}{\frac{1}{\sqrt{N_t^d}}\left[1\exp \left\{-𝒿\varphi \left(f,{\vartheta }_k^d\right)\right\}\dots \exp \left\{-\mathrm{𝒿\varphi }\left(f,{\vartheta }_k^d\right)\left(N_t^d-1\right)\right\}\right]}^T,& \left(7\right)\end{array}$ where

$\varphi \left(f,{\vartheta }_k^d\right)\stackrel{△}{=}2\pi \left(f_c+f\right)\frac{r}{c}{\vartheta }_k^d$ and the superscript T denotes a transpose operator; and v (f, ϑ_k) denotes an array response associated with the frequency and the angle of departure.

For ease of description, considering each coherent time interval, a time parameter t is omitted. In addition, at the mth sub-carrier with the frequency of f_m, let h_k[m]┘h_k(f_m), v_k[m]┘v_k(f_m), and g_k[m]┘g_k(f_m). Thus, a corresponding channel response vector may be expressed as follows:h_k[m]=v_k[m]g_k[m].  (8)(2) Consideration of Downlink Channel Transmission Signals

At the mth sub-carrier, a data vector is s[m]=[s₁[m], s₂[m], . . . , s_K[m]]^T∈□^K×1, where s_k[m] is a transmission symbol for the kth user. Then, a signal transmission vector is x[m]=B[m]s[m]∈□^Nt×1, where B[m] is a hybrid precoding matrix including constant-modulus RF precoders V[m]∈□^Nt×Mt and baseband precoders W[m]=[w₁[m], w₂[m], . . . , w_K[m]]∈□^Mt×K, where w_k[m] is a baseband precoding vector for the kth user. Then, B[m]=V[m]W[m]=[b₁[m], b₂[m], . . . , b_K[m]]∈□^Nt×K is obtained, where b_k[m]=V[m]w_k[m]∈□^Nt×1 is a precoding vector for the kth user.

The signal-to-interference-plus-noise ratio SINR, the rate R_k, and the energy efficiency EE between the satellite and the kth user are respectively defined as follows:

$\begin{array}{cc}{\mathrm{SINR}}_k\left[m\right]\stackrel{△}{=}\frac{{❘b_k^H\left[m\right]h_k\left[m\right]❘}^2}{\sum _{\ell \ne k}{❘b_{\ell }^H\left[m\right]h_k\left[m\right]❘}^2+N_0},& \left(9\right)\end{array}$ $\begin{array}{cc}{R}_k=\sum _{m=1}^M{\Delta }_B{R}_k\left[m\right]=\sum _{m=1}^M{\Delta }_B𝔼\left\{\log \left(1+{\mathrm{SINR}}_k\left[m\right]\right)\right\},& \left(10\right)\end{array}$ $\begin{array}{cc}\mathrm{EE}=\frac{\sum _{k=1}^K{R}_k}{P^{\mathrm{total}}}.& \left(11\right)\end{array}$ where

$P^{\mathrm{total}}=\sum _{k=1}^K\sum _{m=1}^M\xi {b_i\left[m\right]}_2^2+P_i$ is a total transmit power,

$1/\xi$ being the effectiveness of an amplifier, P_t being the static power consumption, and ∥□∥₂ denoting the norm of vector 2; N₀ denotes the noise power; b_l[m] denotes a precoding vector for the lth user; the superscript H is a matrix operator; SINR_k[m] denotes the signal-to-interference-plus-noise ratio of the kth user at the mth sub-carrier; and R_k[m] denotes the rate of the kth user at the mth sub-carrier.2. Sensing Module

A subarray MIMO radar designed in conjunction with a hybrid precoding architecture is considered, and at the mth sub-carrier, the mode of an omnidirectional beam sent by the radar is:Q_m(ϑ)=v_m^H(ϑ)X[m]v_m(ϑ),∀ϑ,  (12)where v_m^H(ϑ)□v(f_m, ϑ) denotes an array response vector with the angle of departure of ϑ, v(f_m, ϑ) denotes an array response associated with the frequency and the angle of departure, ϑ=(ϑ^x, ϑ^y) denotes the angle of departure, ϑ^x and ϑ^y denote the angles of departure in the x and y directions respectively, and the autocorrelation matrix X[m] is defined as follows:X[m]=E{x[m]x^H[m]}=V[m]W[m]W^H[m]V^H[m].  (13)

Assuming that there are P_r≤K detection targets, an optimal subarray radar precoder may be expressed as follows:B_rad[m]=blkdiag{u₁[m], u₂[m], . . . , u_Pt[m]}∈□^Nt×Pr,  (14)where u_p[m]∈□^Nt/Pr×1 denotes elements at corresponding positions in v_p[m], blkdiag{□} denotes a block diagonal array, p∈{1,2, . . . , P_r}, v_p[m] denotes an array response associated with the frequency and the angle of departure, and P_r denotes the number of the targets.3. Design of a Hybrid Precoder Sensing Beam Squint

A hybrid precoder sensing beam squint is designed for the wideband downlink satellite massive MIMO integrated sensing and communication system, so as to ensure the radar sensing performance while seeking maximum energy efficiency of communication, where the following optimization problem P₁ is considered:

$\begin{array}{cc}{𝒫}_1:\underset{{\left\{V❘m\right\},W\left[m\right],U\left[m\right]\}}_{m=1}^M}{\mathrm{maximize}}\frac{\sum _{k=1}^K{R}_k}{P^{\mathrm{total}}}& \left(15\right)\end{array}$ $\begin{array}{cc}s.t.& \sum _{k=1}^K\sum _{m=1}^M{V\left[m\right]w_k\left[m\right]}_2^2\le P,\\ & V\left[m\right]\in 𝒮,\forall m,\\ & {V\left[m\right]W\left[m\right]-B_{\mathrm{rad}}\left[m\right]U\left[m\right]}_F^2\le \epsilon ,\forall m,\\ & U\left[m\right]U^H\left[m\right]=I_{P_r},\forall m,\end{array}$

In the foregoing formula, P denotes the power budget; U[m] is an auxiliary unitary matrix introduced at the mth sub-carrier, which enables the optimal radar precoder and the hybrid precoder to match in dimensions, and this operation does not affect the beam mode of the radar; ε is an Euclidean distance tolerance term between the digital/analog hybrid precoder and the radar precoder (capable of rotation); I_Pr is a unit matrix of the order P_r×P_r; and ∥_∥_F denotes the Frobenius-norm of a matrix. In addition, S□{S_FC, S_PC} denotes the constraints the analog precoders need to satisfy, where specifically speaking, S_FC, S_PC respectively denote the constraints which the analog precoders having fully connected and partially connected structures need to satisfy, that is:

$\begin{array}{cc}{𝒮}_{\mathrm{PC}}\stackrel{△}{=}\left\{V❘❘{\left[V\right]}_{i,j}❘=1,\forall i,j\right\},& \left(16\right)\end{array}$ $\begin{array}{cc}{𝒮}_{\mathrm{PC}}\stackrel{△}{=}\left\{V❘❘{\left[V\right]}_{i,j}❘=1,\forall i,\forall j=\lceil \frac{i}{N_g}\rceil \right\},& \left(17\right)\end{array}$ where N_g=N_t/M_t denotes the number of groups.

Step 1: For the optimization problem P₁, the product of the analog and digital precoders is regarded as a whole and irrelevant constraints are disregarded for the moment, to obtain a fully digital precoding problem P₂:

$\begin{array}{cc}{𝒫}_2:\underset{{\left\{B\left[m\right]\right\}}_{m=1}^M}{\mathrm{maximize}}\frac{\sum _{k=1}^K{R}_k}{P^{\mathrm{total}}}& \left(18\right)\end{array}$ $s.t.\sum _{k=1}^K\sum _{m=1}^M{b_k\left[m\right]}_2^2\le P.$

Step 2: Because it is difficult to estimate an accurate value of R_k[m], considering statistical properties of wave propagation, its tight bound is used as a replacement, namely:

$\begin{array}{cc}{R}_k\left[m\right]\le {\stackrel{\_}{R}}_k\left[m\right]\stackrel{△}{=}\log \left(1+\frac{{\gamma }_k{❘v_k^H\left[m\right]b_k\left[m\right]❘}^2}{\sum _{\ell \ne k}{\gamma }_k{❘v_k^H\left[m\right]b_{\ell }\left[m\right]❘}^2+N_0}\right).& \left(19\right)\end{array}$

Step 3: Let B⁽ⁱ⁾={B⁽ⁱ⁾[m]}_m=1^M be a precoding matrix set of all the sub-carriers, and the problem P₂ is transformed into a series of sub-problems P₃⁽ⁱ⁾, i=1,2, . . . by means of the Dinkelbach algorithm, where i=1, 2, . . . :

$\begin{array}{cc}{P}_3^{\left(i\right)}:\underset{{ℬ}^{\left(i\right)}}{\mathrm{maximize}}F\left(B^{\left(i\right)},{\eta }^{\left(i\right)}\right)=\sum _{k=1}^K{\stackrel{\_}{R}}_k\left(B^{\left(i\right)}\right)-{\eta }^{\left(i\right)}{P}^{\mathrm{total}}\left(B^{\left(i\right)}\right)& \left(20\right)\end{array}$ $s.t.\sum _{k=1}^K\sum _{m=1}^M{b_k^{\left(i\right)}\left[m\right]}_2^2\le P.$ where the auxiliary variable η⁽ⁱ⁾ meets the following equation:

$\begin{array}{cc}{\eta }^{\left(i\right)}=\frac{\sum _{k=1}^K{\stackrel{\_}{R}}_k\left(B^{\left(i-1\right)}\right)}{P^{\mathrm{total}}\left(B^{\left(i-1\right)}\right)}.& \left(21\right)\end{array}$

Step 4: The ith sub-problem is taken into consideration, and the serial number i is omitted for convenience. Let b_k[m]=b_k,m and v_k[m]=v_k,m, and then the problem P₃⁽ⁱ⁾ may be expressed as follows:

$\begin{array}{cc}{P}_3:\underset{ℬ}{\mathrm{maximize}}F\left(ℬ\right)=\sum _{k=1}^K\sum _{m=1}^M\log \left(1+\frac{{\gamma }_k{❘v_{k,m}^H{b}_{k,m}❘}^2}{\sum _{\ell =k}{\gamma }_k{❘v_{k,m}^H{b}_{k,m}❘}^2+N_0}\right)-\eta \left(\xi {b_{k,m}}_2^2+P_1\right)& \left(22\right)\end{array}$ $s.t.\sum _{k=1}^K\sum _{m=1}^M{b_{k,m}}_2^2\le P.$

Step 5: By introducing the auxiliary variable λ={λ_k,m}_k=1,m=1^K,M and by means of Lagrangian dual transformation, the foregoing problem is transformed into P₄:

$\begin{array}{cc}{P}_4:\underset{ℬ,\lambda }{\mathrm{maximize}}F\left(ℬ,\lambda \right)=\sum _{k=1}^K\sum _{m=1}^M\log \left(1+{\lambda }_{k,m}\right)+\left(1+{\lambda }_{k,m}\right)\frac{{\gamma }_k{❘v_{k,m}^H{b}_{k,m}❘}^2}{\sum _{\ell =1}^K{\gamma }_k{❘v_{k,m}^H{b}_{\ell ,m}❘}^2+N_0}-{\lambda }_{k,m}-\eta \left(\xi {b_{k,m}}_2^2+P_1\right)& \left(23\right)\end{array}$ $s.t.\sum _{k=1}^K\sum _{m=1}^M{b_{k,m}}_2^2\le P.$

It should be noted that, when B is fixed, F (B, λ) is a concave function for the variable λ_k,m; and let ϑF/ϑλ_k,m=0, to obtain:

$\begin{array}{cc}{\lambda }_{k,m}^{\mathrm{opt}}=\frac{{\gamma }_k{❘v_{k,m}^H{b}_{k,m}❘}^2}{\sum _{\ell \ne k}{\gamma }_k{❘v_{k,m}^H{b}_{\ell ,m}❘}^2+N_0}.& \left(24\right)\end{array}$

Step 6: By introducing the auxiliary variable ρ={ρ_k,m}_k=1,m=1^K,M and by means of quadratic transformation, the problem P₄ is transformed into:

$\begin{array}{cc}{P}_5:\underset{B,\lambda ,\rho }{\mathrm{maximize}}F\left(B,\lambda ,\rho \right)& \left(25\right)\end{array}$ $s.t.\sum _{k=1}^K\sum _{m=1}^M{b_{k,m}}_2^2\le P.$ $\begin{array}{cc}\mathrm{where}:& \left(26\right)\end{array}$ $F\left(B,\lambda ,\rho \right)=\sum _{k=1}^K\sum _{m=1}^M\log \left(1+{\lambda }_{k,m}\right)-{\lambda }_{k,m}+2\sqrt{\left(1+{\lambda }_{k,m}\right){\gamma }_k}\Re \left\{b_{k,m}^H{v}_{k,m}{\rho }_{k,m}\right\}-{❘{\rho }_{k,m}❘}^2\left(\sum _{\ell =1}^K{\gamma }_k{❘v_{k,m}^H{b}_{\ell ,m}❘}^2+N_0\right)-\eta \left(\xi {b_{k,m}}_2^2+P_1\right).$ $\begin{array}{cc}\mathrm{Let}\partial F/\partial {\rho }_{k,m}=0,\mathrm{to}\mathrm{obtain}:& \left(27\right)\end{array}$ ${\rho }_{k,m}^{\mathrm{opt}}=\frac{\sqrt{\left(1+{\lambda }_{k,m}\right){\gamma }_k}{v}_{k,m}^H{b}_{k,m}}{\sum _{\ell =1}^K{\gamma }_k{❘v_{k,m}^H{b}_{\ell ,m}❘}^2+N_0}.$

Step 7: It is noted that when (η, λ, ρ) is fixed, the target function of the problem P₅ is convex for the variable b_k,m; and then the Lagrangian operator method may be used for evaluation. Specifically, the Lagrange multiplier t is introduced, and then the Lagrange function of the problem P₅ may be expressed as follows:

$\begin{array}{cc}L\left(B,\lambda ,\rho ,t\right)=F\left(B,\lambda ,\rho \right)+t\left(\sum _{k=1}^K\sum _{m=1}^M{b_{k,m}}_2^2-P\right).& \left(28\right)\end{array}$

From KKT conditions, the following formulas can be obtained:

$\begin{array}{cc}{b}_{k,m}^{\mathrm{opt}}={\left(\sum _{\ell =1}^K{❘{\rho }_{\ell ,m}❘}^2{\gamma }_{\ell }{v}_{\ell ,m}{v}_{\ell ,m}^H+\left(\mathrm{\eta \xi }+t\right)I\right)}^{-1}\sqrt{\left(1+{\lambda }_{k,m}\right){\gamma }_k}{\rho }_{k,m}{v}_{k,m},& \left(29\right)\end{array}$ $\begin{array}{cc}t=\arg \underset{t\ge 0}{\min }\sum _{k=1}^K\sum _{m=1}^M{b_{k,m}^{\mathrm{opt}}}_2^2\le P.& \left(30\right)\end{array}$

Step 8: For the mth sub-carrier, after an equivalent fully digital pre-coding matrix B_com[m] is obtained, a weighting coefficient ζ is introduced to weigh the performance of communication and sensing modules, where a corresponding minimization problem for a weighted sum is:

$\begin{array}{cc}{Q}_i^m:\underset{V\left[m\right],W\left[m\right],U\left[m\right]}{\mathrm{minimize}}f\left(V\left[m\right],W\left[m\right],U\left[m\right]\right)=\zeta {V\left[m\right]W\left[m\right]-B_{\mathrm{com}}\left[m\right]}_F^2+\left(1-\zeta \right){V\left[m\right]W\left[m\right]-B_{\mathrm{rad}}\left[m\right]U\left[m\right]}_F^2& \left(31\right)\end{array}$ $\begin{array}{cc}s.t.& V\left[m\right]\in S,\forall m,\\ & {B_{\mathrm{com}}\left[m\right]}_F^2={V\left[m\right]W\left[m\right]}_F^2,\\ & U\left[m\right]U^H\left[m\right]=I_{P_r},\forall m,\end{array}$ where ζ denotes the weight. For any sub-carrier m, analog and digital precoding vectors can be obtained by means of iterative solution, and the mark number m is omitted in the following description.

Step 9: For the analog precoders having the fully connected structure: (4) for the fixed V and W, the problem Q₁ is transformed into:

$\begin{array}{cc}{Q}_2:\underset{U}{\mathrm{minimize}}{\mathrm{VW}-B_{\mathrm{rad}}U}_F^2& \left(32\right)\end{array}$ $s.t.{\mathrm{UU}}^H=I_{P_r},$ A solution to the foregoing problem can be obtained by means of singular value decomposition, namely:U=QI_Pr×KR,  (33)where Q and R are results after singular value decomposition is performed for B_rad^HVW, that is, QΣR=B_rad^HVW, Q and R being unitary matrixes and Σ being a diagonal matrix; and I_Pr×K=[I_Pr,0] is a sparse matrix.

(5) For the fixed V and U, the problem Q₁ is transformed into:

$\begin{array}{cc}{Q}_3:\underset{W}{\mathrm{minimize}}\zeta {\mathrm{VW}-B_{\mathrm{com}}}_F^2+\left(1-\zeta \right){\mathrm{VW}-B_{\mathrm{rad}}U}_F^2& \left(34\right)\end{array}$ $s.t.{B_{\mathrm{com}}}_F^2={\mathrm{VW}}_F^2,$

It is noted that, for the problem Q₃, its target function is expressed as a weighted sum of two F norms. Let the auxiliary matrixes A=[√{square root over (ζ)}V^T, √{square root over (1−ζ)}V^T]^T∈□^2Nt×Mt and C=[√{square root over (ζ)}B_com^T, √{square root over (1−ζ)}U^TB_rad^T]^T∈□^2Nt×K, A^HA=V^HV can be easily deduced. Thus, the problem Q₃ can be transformed into:

$\begin{array}{cc}{Q}_4:\underset{W}{\mathrm{minimize}}{\mathrm{AW}-C}_F^2& \left(35\right)\end{array}$ $s.t.{B_{\mathrm{com}}}_F^2={\mathrm{AW}}_F^2,$ Then, the digital precoder W can be updated as follows:

$\begin{array}{cc}W={\left(A^{H}A\right)}^{-1}{A}^{H}C={\left(V^{H}V\right)}^{-1}{A}^{H}C,& \left(36\right)\end{array}$ $\begin{array}{cc}W=\frac{{B_{\mathrm{com}}}_F}{{\mathrm{VW}}_F}W.& \left(37\right)\end{array}$

(6) Let G=[√{square root over (ζ)}W, √{square root over (−1ζ)}W]∈□^M1×2K and T=[√{square root over (ζ)}B_com, √{square root over (1−ζ)}B_radU]∈□^Nt×2K be auxiliary matrixes, and for the fixed W and U, the problem Q₁ is transformed into:

$\begin{array}{cc}{Q}_5:\underset{V}{\mathrm{minimize}}{\mathrm{VG}-T}_F^2& \left(38\right)\end{array}$ $s.t.V\in {𝒮}_{\mathrm{FC}},$

Let the auxiliary matrix Y=GG^H, where its maximum characteristic value is λ_max(Y); and then the problem Q₅ is transformed into:V=exp{−ø∠Z^T},  (39)where Z=GT^H−(Y−λ_max(Y)I_Mt)V^H is an auxiliary matrix, and ∠ denotes an operator for evaluation of an angle.

Steps (1) to (3) are repeated till the target function f converges.

Step 10: For the analog precoders having the partially connected structure, the (i,j)th element thereof is [V]_i,j=exp{øϕ_i,j}, and ∀i, j=┌i/N_g┐, where ┌□┐ denotes an operator for evaluation of an upper bound, ϕ_i,j is an angle of the (i,j)th element in the matrix, and a corresponding analog precoding matrix meets

${\mathrm{VW}}_F^2=N_g{W}_F^2={B_{\mathrm{com}}}_F^2.$

(4) For the fixed V and W, the problem Q₁ is transformed into:

$\begin{array}{cc}{Q}_6:\underset{U}{\mathrm{minimize}}{\mathrm{VW}-B_{\mathrm{rad}}U}_F^2& \left(40\right)\end{array}$ $s.t.{\mathrm{UU}}^H=I_{P_r},$ A solution to the foregoing problem can be obtained by means of singular value decomposition, namely:U=QI_Pr×KR,  (41)where Q and R are results after singular value decomposition is performed for B_rad^HVW, that is, QΣR=B_rad^HVW, Q and R being unitary matrixes and Σ being a diagonal matrix; and I_Pr×k=[I_pr,0] is a sparse matrix.

(5) Let A=[√{square root over (ζ)}V^T, √{square root over (1−ζ)}V^T]^T∈□^2Nt×Mt and C=[√{square root over (ζ)}B_com^T, √{square root over (1−ζ)}U^TB_rad^T]^T∈□^2Nt×K be auxiliary matrixes, and for the fixed V and U, the problem Q₁ may be transformed into:

$\begin{array}{cc}{Q}_7:\underset{W}{\mathrm{minimize}}{A^{H}C-W}_F^2& \left(42\right)\end{array}$ $s.t.{W}_F=\frac{{B_{\mathrm{com}}}_F}{\sqrt{N_g}},$ Then, the digital precoder W can be updated as follows:

$\begin{array}{cc}W=\frac{{B_{\mathrm{com}}}_F}{\sqrt{N_g}}\frac{A^{H}C}{{A^{H}C}_F}.& \left(43\right)\end{array}$

(6) Let the auxiliary matrixes a=[√{square root over (ζ)}[B_com]_i,:, √{square root over (1−ζ)}[B_radU]_i,:] and p=[√{square root over (ζ)}[W]_j,:, √{square root over (1−ζ)}[W]_j,:], where [□]_i,: denotes the ith row of the matrix and [□]_j,: denotes the jth row of the matrix; and for the fixed W and U, the problem Q₁ is transformed into:

$\begin{array}{cc}{Q}_8\text{:}\underset{v}{\mathrm{minimize}}{a-\exp \left\{{\mathrm{⌀\varphi }}_{i,j}\right\}p}_2^2& \left(44\right)\end{array}$ $s.t.V\in S_{\mathrm{PC}},$ Then, a solution to this problem may be expressed as follows:

$\begin{array}{cc}{\left[V\right]}_{i,j}=\exp \left\{\mathrm{⌀\angle }\left({\mathrm{ap}}^H\right)\right\},\forall i,\forall j=\lceil \frac{i}{N_g}\rceil .& \left(45\right)\end{array}$ Steps (1) to (3) are repeated till the target function f converges.

During the dynamic movement of the satellite and the user terminals as well as the targets, with the change in the statistical properties of wave propagation between the satellite and the user terminals as well as the targets, the foregoing integrated sensing and communication hybrid precoding process is dynamically implemented, to form an updated integrated sensing and communication hybrid precoding method.

The above merely describes preferred embodiments of the present disclosure. It should be noted that, several improvements and modifications may be made by those of ordinary skill in the art without departing from the principle of the present disclosure, and these improvements and modifications should also be construed as falling within the protection scope of the present disclosure.

Claims

1. A transmit method based on satellite massive Multiple-Input Multiple-Output (MIMO) integrated sensing and communication, comprising: providing a satellite end with a massive MIMO antenna array which simultaneously serves multiple users and detects multiple targets, wherein communication and sensing use the same spectrum resources and the same hardware platform, and integrated sensing and communication is implemented by transmitting a signal to focus on communication or sensing;estimating, by the satellite end, statistical status information of electromagnetic wave propagation according to received uplink and downlink pilot signals, wherein for a communication process, the statistical status information of electromagnetic wave propagation is a channel gain and a channel direction vector between the satellite end and user terminals;for a sensing process, configuring the statistical status information of electromagnetic wave propagation with angles of departure of the targets;according to the statistical status information of electromagnetic wave propagation, transmitting, by the satellite end, a directional beam to a detection target and a downlink signal to each user terminal by means of integrated sensing and communication precoding; andduring dynamic movement of the satellite and the user terminals as well as the targets, updating the integrated sensing and communication precoding with a change in the statistical status information of electromagnetic wave propagation between the satellite and the user terminals as well as the targets.

2. The transmit method based on satellite massive MIMO integrated sensing and communication according to claim 1, wherein in the simultaneously implementing communication and sensing, performance of communication and sensing is weighed by introduction of a weighting coefficient.

3. The transmit method based on satellite massive MIMO integrated sensing and communication according to claim 2, wherein the integrated sensing and communication precoding comprises the following steps: to ensure the-radar sensing performance while seeking maximum energy efficiency of communication, establishing an optimization problem based on equation (1):