Embodiments of the present invention generally relate to transceiver spectrum sharing and, more particularly, to a method and system for optimizing transceiver spectrum sharing.
Assured spectrum access is a growing challenge for all sorts of transceivers, including both incumbent radars and communication systems. These challenges will continue to grow as mobile data traffic increases and requires the need for more bandwidth. One example of this spectrum access paradigm in the United Sates is the Citizens Broadband Radio Service (CBRS) at 3.5 GHz, which promotes spectrum sharing between Long-Term Evolution (LTE) (a so-called “secondary user”) and radar (a so-called “primary user”). Another example considers the Federal Communications Commission (FCC) auction of the advanced wireless service 3 (AWS-3) bands. In most circumstances, the incumbent users of the AWS-3 bands must either vacate the band or share the band with the new licensed users. Other frequency bands are being considered for auction that could have a tremendous impact on government radar systems, which are typically the incumbent or primary user. Ideally future radars will have the capability to coexist with secondary (or lower priority) RF users and with communication systems that have equal rights to the band while maintaining high-performance requirements of both primary and secondary user equipment.
Solutions to these spectrum challenges include cognitive radar for spectrum sharing. Spectrum sharing approaches are grouped into categories of coexistence and cooperation. Coexistence approaches monitor the spectrum to mitigate mutual interference. The classic coexistence example is cognitive radio for dynamic spectrum access (DSA). The cognitive radio implements spectrum sensing to monitor the spectrum for primary user activity. The underutilized spectrum is then dynamically accessed when the primary user is inactive (temporal spectrum access). Other coexistence approaches implement a sense-and-avoid strategy, which changes the operational frequency of the radar to avoid RF emitters in the spectrum. An example of this approach is the spectrum sensing, multi-objective optimization (SSMO) technique. SSMO maximizes multiple objective functions to identify the optimal frequency allocation based on spectrum sensing information and has been shown to maximize radar performance while mitigating mutual interference.
Cooperative approaches consider a co-design strategy between the radar and communication system that follow a common protocol. Some approaches combine the functionality of radar and radio into one “radar-communications node,” which maximizes joint performance. Other approaches consider radar protection zones with power allocation for in-band operation of the radar and communication system. These approaches examine the harmful interference between systems, the minimum distance (or power level) to mitigate harmful interference and apply methods to attenuate communication system power to prevent mutual interference.
Currently available coexistence and cooperative techniques do not optimally mitigate the interference between primary and secondary user equipment. Therefore, there is a need in the art for a comprehensive system to optimize spectrum sharing among transceivers, especially among radars and communications systems.
Embodiments of the invention include a cooperative spectrum sharing model that jointly optimizes multiple radar and communication system parameters for improved frequency agility and performance while mitigating mutual interference between secondary radio-frequency (RF) users. Spectrum sensing is implemented to form a power spectral estimate of the electromagnetic environment (EME) to identify secondary user equipment. Multi-objective optimization then adjusts the output power, center frequency, and bandwidth parameters of the primary user equipment to maximize range resolution, signal to interference plus noise ratio (SINR), and channel capacity.
So that the manner in which the above recited features of the present invention can be understood in detail, a more particular description of the invention, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. It is to be noted, however, that the appended drawings illustrate only typical embodiments of this invention and are therefore not to be considered limiting of its scope, for the invention may admit to other equally effective embodiments.
Embodiments of the invention include a method and system for optimizing spectrum sharing among transceivers. In one embodiment, the system comprises a spectrum sensing system that is coupled to certain controllable transceivers (primary user equipment) such as communications systems and radar systems. The spectrum sensing system monitors a relevant spectrum for background interference, secondary user equipment transmissions, and primary user equipment transmissions. An optimization method analyses the spectrum and adapts the utilization of the spectrum by the primary user equipment to optimize sharing of the spectrum with the secondary users.
The spectrum sharing scenario 100, illustrated in
The radar 102 and target 108 are located at positions P1 and P0, respectively, separated by a distance of R10. The CBS 106 and UE 104 are located at positions P2 and P3, respectively, separated by a distance of R23. R13 indicates the distance between the radar 102 and the UE 104, while R21 indicates the distance between the radar 102 and the CBS 106. In this scenario, the capacity of the downlink channel is examined, and the UE 104 is positioned at the minimal separation distance to the radar 102 (close as possible), denoted as R13, within the main beam of the radar 102. This distance represents the maximum interference possible from the radar 102 to the UE 104, i.e., the worst-case scenario.
The scenario 100 of
A spectrum sensing system 110 shown in
The SS-MO solution is found using a multiobjective genetic algorithm as, for example, described in A. Konak, D. Coitb, and A. Smith, “Multi-Objective Optimization Using Genetic Algorithms: A Tutorial,” Reliability, Engineering, and System Safety, vol. 91, no. 9, pp. 992-1007, September 2006, hereby incorporated by reference in its entirety. There are many genetic algorithms that may find use in various embodiments of the invention including, but not limited to: Multi-objective Genetic Algorithm (MOGA), Niched Pareto Genetic Algorithm (NPGA), Weight-based Genetic Algorithm (WBGA), Random Weighted Genetic Algorithm (RWGA), Nondominated Sorting Genetic Algorithm (NSGA), Strength Pareto Evolutionary Algorithm (SPEA), improved SPEA (SPEA2), Pareto-Archived Evolution Strategy (PAES), Pareto Envelope-based Selection Algorithm (PESA), Region-based Selection in Evolutionary Multiobjective Optimization (PESA-II), Fast Nondominated Sorting Genetic Algorithm (NSGA-II), Multi-objective Evolutionary Algorithm (MEA), Micro-GA, Rank-Density Based Genetic Algorithm (RDGA), and Dynamic Multi-objective Evolutionary Algorithm (DMOEA).
One specific example of a genetic algorithm is the NSGA-II technique described in K. Deb, A. Pratap, S. Agarwal, T. Meyarivan, “A fast and elitist multiobjective genetic algorithm: NSGA-II,” IEEE Transactions on Evolutionary Computation, vol. 6, no. 2, pp. 182-197, April 2002, hereby incorporated by reference in its entirety. NSGA-II sorts a population of individuals, where each individual represents a decision variable with a corresponding solution. The solution for each individual is found using objective functions. After an initial parent population is randomly generated, NSGA-II implements: 1) crossover and mutation; 2) a formation of an elite population; and 3) a population sort and rank procedure. Each iteration of this procedure produces the next generation of samples, i.e., the children, within the population. Simulated binary crossover (SBX) is used for the crossover procedure with parameter ηc. A large ηc produces children very similar to the parents, where a small ηc produces dissimilar children. Polynomial mutation is used for the mutation process with parameter ηm, a variable that controls the similarity between the original and mutated individual (with properties similar to ηc). An elite population of M individuals is then formed by combining the parent and child generations, which is then sorted and ranked using the non-dominated procedure. The goal of the genetic algorithm is to evolve this population over T generations such that the decision variables converge to the optimal solution.
The decision variable vector is defined as x={x1, x2, x3, x4, x5, x6}. The variable x1=P1 is the radar transmitter power, where 0≤P1≤P1,max and P1,max is the max available power. The radar bandwidth is defined as x2=β1(i)=ΔB, where iϵ {1, . . . N}. Note that β1(i)=B, the full bandwidth solution, when i=N and β1(i)=ΔB, the frequency resolution, when i=1. x3=δ1(j)=fj ϵF is the lower, or start, frequency of the linear frequency modulated (LFM) waveform, where jϵ {1, . . . N}. The lower frequency is used in this development, as opposed to the center frequency δ1(j)+δ1(j)/2, to make the mathematical development more convenient. Note that β1(i)+δ1(j)≤B, i.e., the operational band of the radar cannot exceed the upper limit of the baseband. The CBS transmitter power is defined as x4=P2, where 0≤P2≤P2,max and P2,max is the max available power. x5=β2(k) is the CBS and UE bandwidth of operation, where kϵ {1, . . . K}. The variable x6=δ2(l)=flϵ F is the lower frequency of the CBS and UE bandwidth of operation, where lϵ{1, . . . N}.
The radar SINR objective function is defined as
Z1=P1G12λ2σNPτβ1(i)/[L1(4π)3R104(l21(P2,i,j,k,l)+Γ1(i,j))] (defined and hereinafter referred to as “Equation 1”)
where G1 is the radar antenna gain, λ is wavelength, σ is the target radar cross section, NP is the number of pulses per coherent processing interval (CPI), L1 is the radar system loss, τ is pulse width, and τ β1>100 is the time-bandwidth product for the linear frequency modulated waveform. The variable
is the interference and noise power estimate for all contiguous sub-bands in the spectrum produced by the secondary users as seen by the radar. The radar receiver noise factor is defined as Nf1, but the receiver noise power is inherently estimated in Equation 2 by summing the noise floor for different bandwidth combinations. The interference from the eNodeB to the radar is defined as
l21(P2,i,j,j,l)=P2G1G2ψ21/FDR(i,j,k,l) (defined and hereinafter referred to as “Equation 3”)
where G2 is the CBS antenna gain, Ψ21 is the path loss between the CBS and the radar, and FDR(i, j, k, l) is the Frequency Dependent Rejection (FDR) that measures the interference rejection between the radar and CBS. The FDR offset is based on the co-channel and adjacent channel interference between the two systems. Only co-channel interference is of interest. Note that FDR(i,j,k,l) is dependent on the decision variables, hence more interference occurs when the operating sub-bands of the radar and eNodeB overlap.
The second objective function is the radar range resolution defined as
ΔR=c/[2β1(i)], (defined and hereinafter referred to as “Equation 4”)
where c is the speed of light. A small resolution cell size is advantageous for separating closely spaced point targets in range or extracting features from extended targets. Ideally, the radar would occupy β1(N)=B in order to maximize Equation 4, but that decision would decrease Equation 1 (SINR) due to the interference generated by Equation 2 and Equation 3.
The final objective function is the UE capacity modeled as
Z3=β2(k)log2[1+Φ3], (defined and hereinafter referred to as “Equation 5”)
where
Φ3=P2G2G3ψ/[L2(l13(P1,i,j)+Γ(k,l))] (defined and hereinafter referred to as “Equation 6”)
is the SINR of the UE 104. G3 is the antenna gain of the UE 104 and Ψ23 is the path loss between the CBS 106 and the UE 104. The variable
is the interference and noise power estimate for all contiguous sub-bands in the spectrum produced by the secondary RF emitters as seen by the UE 104. The UE noise factor is defined as Nf3. The interference from the radar to the UE 104 is defined as
l13(P1,i,j)=P1G1G3ψ13/[L1L3 FDR(i,j,k,l)] (defined and hereinafter referred to as “Equation 8”)
where L3 is the UE system loss and ψ13 is the path loss between the radar and the UE.
The goal of the NSGA-II approach is to find the decision vector x*={x1*, x2*, x3*, x4*, x5*, x6*} that maximizes the objective functions in Equation 1, Equation 4, and Equation 5:
Z(x*)={Z1(x*), Z2(x*), Z3(x*)} (defined and hereinafter referred to as “Equation 9”)
in the solution space X subject to the constraints Z1(x*)≥Z1,min and Z2(x*)≤Z2,min, and Z3(x*)≤Z3,min, where Z1,min, Z2,min, and Z3,min are the boundary conditions for minimum. SINR, bandwidth, and capacity respectively. The solution in Equation 9 is considered feasible if it satisfies these boundary conditions
Aspects of this invention have been previously disclosed by the inventors in a paper titled “Joint Radar and Communication System Optimization for Spectrum Sharing,” which was presented at the 2019 IEEE Radar Conference, Boston Mass., 22-26 Apr. 2019. This paper is herein incorporated by reference in its entirety.
While the foregoing is directed to embodiments of the present invention, other and further embodiments of the invention may be devised without departing from the basic scope thereof, and the scope thereof is determined by the claims that follow.
The invention described herein may be manufactured, used and licensed by or for the U.S. Government.
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20210135703 A1 | May 2021 | US |