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CN109361442A - Non-orthogonal multiple access downlink transmission method for air array communication - Google Patents

Non-orthogonal multiple access downlink transmission method for air array communication
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CN109361442A
CN109361442ACN201811231452.5ACN201811231452ACN109361442ACN 109361442 ACN109361442 ACN 109361442ACN 201811231452 ACN201811231452 ACN 201811231452ACN 109361442 ACN109361442 ACN 109361442A
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base station
space
airborne
signal
ground
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肖振宇
曹先彬
罗喜伶
刘凯
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Beihang University
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Beihang University
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Abstract

Translated fromChinese

本发明公开了临空阵列通信非正交多址接入下行传输方法,属于临空通信技术领域。首先构建通信场景,地面基站对临空基站发送的信号进行叠加发射,叠加信号形成混合信号;地面基站和每个临空基站之间进行毫米波定向通信,得到与各临空基站的信道响应向量;选择临空基站最强路径上的信道响应向量作为有效信道响应向量;利用波束赋形向量w对有效信道增益做出相应排序,针对空基1解码发射信号s2并消除再解码发射信号s1,空基2解码发射信号s2得到各空基的可达率,当可达率之和达到最大化时设计联合功率分配及波束赋形需满足的约束条件。对约束条件求解,得到各临空基站相应的功率分配和地面基站的波束赋形方案。本发明有效提高频谱效率,计算复杂度较低。

The invention discloses a non-orthogonal multiple access downlink transmission method for airport array communication, and belongs to the technical field of airport communication. First, a communication scenario is constructed. The ground base station superimposes and transmits the signals sent by the airport base station, and the superimposed signals form a mixed signal; millimeter-wave directional communication is performed between the ground base station and each airport base station, and the channel response vector with each airport base station is obtained. ; Select the channel response vector on the strongest path of the airborne base station as the effective channel response vector; use the beamforming vector w to sort the effective channel gain accordingly. Space base 1 decodes the transmitted signal s2 and cancels and decodes the transmitted signal s1 . Space base 2 decodes the transmitted signal s2 to obtain the reachability of each space base. When the sum of the reachability ratios is maximized, the joint power allocation and beams are designed Constraints to be satisfied. The constraints are solved, and the corresponding power allocation of each airborne base station and the beamforming scheme of the ground base station are obtained. The invention effectively improves the spectral efficiency and has low computational complexity.

Description

Face sky array communications non-orthogonal multiple access downlink transmission method
Technical field
The invention belongs to face sky field of communication technology, specifically a kind of sky array communications non-orthogonal multiple access downlink of facing is passedTransmission method.
Background technique
With the development of information technology, the growth of communication requirement amount exponentially utilizes near space dirigible and low latitudeUnmanned plane effectively can supplement and improve existing communication system as null base station services terrestrial user is faced.Due to dirigible and nothingIt is man-machine that all there is good mobility, it can fast implement the traffic demands for meeting specific region, such as remote districtsCommunication support, the communication service of emergency communication and high business demand area in the case of natural calamity.
On the one hand, growing communication requirement is unable to satisfy since bandwidth limits in traditional microwave frequency range.And millimeterWave (30-300GHz) possesses frequency spectrum resource abundant, shows huge advantage and potentiality increasing spectral bandwidth this aspect,The growth of bandwidth directly will effectively improve the capacity of communication system.However, due to millimeter wave propagation loss with higher,Face in empty communication at a distance and faces huge challenge.
The size of antenna and the wavelength direct proportionality of carrier wave in usual mobile communication, millimeter wave is due in higherFrequency band, wavelength are less than the wavelength of traditional communication band, thus the size of antenna can design it is smaller.ThisSample, identical space size can accommodate more antennas, can also be easier deployment aerial array, with reach enter it is moreThe purpose of the array gain of (Multiple-Input Multiple-Output, MIMO) out.So-called mimo systems, justIt is traditional single antenna transmissions to be become array antenna, transmitting terminal and receiving end all respectively carry out reasonable wave beam forming, so thatThe beam gain of multiple antennas is respectively directed to hair/receiving end, this makes it possible to realize array gain, in the feelings for not changing total transmission powerThe intensity for increasing receiving end received signal under condition can effectively resist the range attenuation faced in empty communication.
On the other hand, it with the raising of number of users and communication requirement, needs to increase the quantity for facing sky aircraft, ground masterBase station needs effectively to control and communicate to facing null base station real-time perfoming, while facing null base station and wanting the multiple users in real time service ground.In traditional method, the base station of single radio frequency can only connect one in same time domain/frequency domain/code domain and face null base station or user, thisJust greatly limit the access quantity for facing null base station and user.
In millimere-wave band, in order to make up gain loss caused by high propagation attenuation, generally realized using aerial arrayArray gain, in order to meet the needs of low hardware deterioration, using the method for analog beam figuration, all antennas share a radio frequencyLink, and the weight coefficient of each antenna has the long constraint of identical mould.Using a small amount of radio frequency link and large scale array dayLine is accessed by millimeter wave non-orthogonal multiple, ground base station may be implemented when identical/frequency/code resource under connect and multiple face skyBase station, and face null base station may be implemented when identical/frequency/code resource under connect multiple terrestrial users.
Summary of the invention
To solve the above-mentioned problems, the present invention accesses (Non Orthogonal Multiple using non-orthogonal multipleAccess, NOMA) mode, it proposes one kind and faces sky array communications non-orthogonal multiple access downlink transmission method, sent out by designIt penetrates the wave beam forming vector at end while aiming at two long-range receiving ends and distributing different transmitting signal powers for them, thusRealize the purpose maximized up to the sum of rate.
Specific step is as follows:
Step 1: facing sky non-orthogonal multiple access communications system for downlink, constructing ground base station and facing between null base stationCommunication scenes.
Communication scenes include: 1. ground base stations to multiple downlink transfers for facing null base station;2. facing null base station to multiple groundThe downlink transfer of user;3. the downlink transfer that ground base station services multiple low latitude unmanned planes.
For the first ground base station to the scene of multiple downlink transfers for facing null base station, specific building is as follows:
Ground base station has N member aerial array, and 2 single antenna are connected in same time domain/frequency domain/code domain resource block and are remotely facedNull base station, it is respectively space base 1 and space base 2 that two, which are faced null base station,.In ground base station one end, every antenna branch has a phase to turnParallel operation and power amplifier, all power amplifiers have identical scale factor, therefore wave beam forming vector, i.e. antenna power systemThe mould length of each component of number vector is equal, referred to as permanent modular constraint.
Step 2: being directed to the first model of place, ground base station will believe all power normalizations for facing null base station transmissionNumber it is overlapped transmitting;
Superposed signal expression formula are as follows:
siIndicate ground base station to the transmitting signal for facing null base station i transmission, piFor to the transmitting signal power for facing null base station i;I=1,2.
Step 3: superposed signal s by ground base station and after facing the channel response between null base station and antenna noise shapeAt mixed signal, and faces null base station by two and respectively receive;
Face the received mixed signal of null base station 1 are as follows:
Face the received mixed signal of null base station 2 are as follows:
Wherein hiIt is the channel response vector of ground base station and space base i, w indicates the wave beam forming vector under permanent modular constraint,Its permanent modular constraint is that each component mould length is equalN is ground base station antenna number, niIndicate emptyWhite Gaussian noise on base i antenna, mean power are denoted as σ2
Step 4: ground base station uses the uniform linear array antenna of half-wave spacing, and each faces between null base station and carry outMillimeter wave beam communication obtains and respectively faces the channel response vector of null base station;
Ground base station and the channel response vector h for facing null base station iiFormula are as follows:
Wherein λi,lIndicate the complex coefficient of the l articles diameter of space base i, LiIndicate the multipath component total number for facing null base station i,Ωi,lIndicate that cosine value of the l articles diameter in the ground base station angle of departure of space base i, a () indicate the function for being directed toward vector, expressionFormula are as follows:
A (N, Ω)=[ejπ0Ω,ejπ1Ω,ejπ2Ω,…,ejπ(N-1)Ω]
A (N, Ω) depends on the geometry of array antenna;
Step 5: selecting the channel response vector on most strong path as ground base station for each path for facing null base station iWith the efficient channel response vector h for facing null base station ii
hiia(N,Ωi)
Wherein λiIndicate the complex coefficient in the most strong path of space base i, i.e., | λi|≥|λi,l|。
Step 6: using the wave beam forming vector w under permanent modular constraint, the efficient channel gain to null base station is respectively facedCorresponding sequence is made, the decoding priority orders of each space base signal are obtained.
Efficient channel gain depends on channel gain and array gain, and efficient channel gain is lower, and decoding priority is higher;
For efficient channel gainPriority when the signal decoding of space base 2 is higher than the signal of space base 1Decode priority;
For efficient channel gainPriority when the signal decoding of space base 1 is higher than the signal of space base 2Decode priority;
Step 7: being ordered as efficient channel gainSpace base 1 will emit signal s2Preferential decoding is simultaneouslyIt is eliminated in the signal of superposition, further decoding emits signal s1, space base 2, which directly decodes, emits signal s2, obtain the reachable of each space baseRate;The reachable rate of two space bases is calculated separately using shannon formula, as follows:
The reachable rate R of space base 11Are as follows:
The reachable rate R of space base 22Are as follows:
Step 8: when all the sum of reachable rates for facing null base station reach maximization, the distribution of design joint Power and wave beamThe constraint condition that figuration need to meet.
Reach maximization i.e. objective function up to the sum of rate, as follows:
The constraint condition that need to meet is as follows:
p1+p2=P
Wherein riIndicate the minimum reachable rate constraint for facing null base station i;P is the maximum power for facing the transmitting signal of null base station.
Step 9: solving to the constraint condition that need to meet, respectively faced the corresponding power distribution of null base station and ground base stationBeamforming scheme, obtain good performance.
Specific step is as follows:
First, by maximized each the sum of reachable rate for facing null base station, power control and beam gain distribution are split asSubproblem and wave beam forming two sub-problems, and introduce intermediate variableIt is converted.
Under ideal wave beam forming, beam gain meets:
Power control and beam gain distribution subproblem statement as a result, are as follows:
Reach maximization up to the sum of rate are as follows:
The condition that need to meet is as follows:
p1+p2=P
The statement of wave beam forming subproblem are as follows:
Wherein, α is the intermediate variable introduced, so that each component of wave beam forming vector approaches permanent modular constraint condition;[w]iIndicate i-th of element of w;
Then, to after conversion power control and beam gain distribution subproblem solve;
The reachable rate of space base 2 is equal to its minimum reachable rate and constrains when the problem acquires optimal solution, i.e.,
Power control is obtained by derivation and beam gain distributes the optimal solution of subproblem are as follows:
Simultaneously, the wave beam forming subproblem after conversion is solved;
DefinitionWave beam forming subproblem becomes:
Suitable the amount of phase rotation is selected by phase rotationSo thatIt is real number, wave beam forming subproblem is convertedAre as follows:
The convex optimization problem of several standards is further decomposed into, it is corresponding when by search w acquirement optimal solutionPhase,It givesSo that it is become linear restriction multiplied by different phases, obtain the convex optimization problem of a series of standard of equal value:
Wherein M is phase search total number, m=1,2..., M.
It is solved with the convex optimization tool of standard, that solution that α is minimized in all optimization problems is selected to be denoted asThenPower normalization is carried out to wave beam forming vector
Finally, rightPermanent mould normalization is carried out, is keptThe phase invariant of each component uniformly becomes lengthTableIt is as follows up to formula:
Final power distribution and beamforming scheme as a result, respectivelyAnd w*
The present invention has the advantages that
1), one kind faces sky array communications non-orthogonal multiple access downlink transmission method, can double up and face empty communicationIn face null base station/terrestrial user access quantity;
2), one kind faces sky array communications non-orthogonal multiple access downlink transmission method, co-design transmitting terminal wave beam formingPower distribution can effectively improve spectrum efficiency, that is, maximize up to the sum of rate;
3), one kind faces sky array communications non-orthogonal multiple access downlink transmission method, has lower computation complexity, energyEnough realize fast beam figuration and power distribution.
Detailed description of the invention
Fig. 1 is model of place schematic diagram of the ground base station of the present invention to multiple downlink transfers for facing null base station;
Fig. 2 is downlink phased-array antenna structure schematic diagram in the present invention;
Fig. 3 is a kind of flow chart for facing sky array communications non-orthogonal multiple and accessing downlink transmission method of the present invention.
Specific embodiment
Below in conjunction with drawings and examples, the present invention is described in further detail.
One kind of the present invention faces sky array communications non-orthogonal multiple access downlink transmission method, with ground base station to facing null base stationFor downlink transfer, ground base station accessed on same time domain/frequency domain/code domain resource block it is multiple face null base station, in power domainThey are distinguish.Ground base station faces empty signal mixing transmission multiple, respectively faces null base station and is done according to efficient channel gainCorresponding sequence out, channel gain is lower, and priority is higher, and assigned power is also higher.In this manner it is achieved that being adopted in receiving endIt is decoded with serial interference elimination (SIC) method, the high signal priority of priority is decoded, and is each faced null base station and is only needed to decodeThe signal higher than oneself priority, and these strong jammings are cut in mixed signal, finally decode the signal of oneself.By thisNon-orthogonal multiple access way not only increases the quantity for facing null base station, and improves the availability of frequency spectrum.The present invention is this non-Orthogonal access mode is equally applicable to face the downlink transfer scene and ground base station of null base station and terrestrial user while takeIt is engaged in the scenes of multiple low latitude unmanned planes.
As shown in Figure 3, the specific steps are as follows:
Step 1: facing sky non-orthogonal multiple access communications system for downlink, constructing ground base station and facing between null base stationCommunication scenes.
Communication scenes include: 1. ground base stations to multiple downlink transfers for facing null base station;2. facing null base station to multiple groundThe downlink transfer of user;3. the downlink transfer that ground base station services multiple low latitude unmanned planes.
For the first ground base station to the scene of multiple downlink transfers for facing null base station, as shown in Figure 1, specific building is such asUnder:
Ground base station has N member aerial array, and 2 single antenna are connected in same time domain/frequency domain/code domain resource block and are remotely facedNull base station, it is respectively space base 1 and space base 2 that two, which are faced null base station,.As shown in Fig. 2, every antenna branch has in ground base station one endOne phase converter (Phase Shifter) and power amplifier (Power Amplifier, PA), own under normal conditionsPower amplifier have identical scale factor, therefore wave beam forming vector, i.e. antenna weight coefficient vector (Antenna WeightVector, AWV) each component mould length it is equal, referred to as permanent modular constraint (Constant-modulus, CM).
Step 2: being directed to the first model of place, ground base station will believe all power normalizations for facing null base station transmissionNumber it is overlapped transmitting;
Ground base station is s to the power normalization signal that space base i (i=1,2) is senti, wherein the expectation of each signalSignal siTransmission power be pi, ground base station is by s1And s2Superposition transmitting, expression formula are as follows:
Step 3: superposed signal s by ground base station and after facing the channel response between null base station and antenna noise shapeAt mixed signal, and faces null base station by two and respectively receive;
2 space base received signals are respectively as follows:
y1To face the received mixed signal of null base station 1;y2To face the received mixed signal of null base station 2.
Wherein hiIt is the channel response vector of ground base station and space base i, w indicates the wave beam forming vector under permanent modular constraint,Its permanent modular constraint is that each component mould length is equalN is ground base station antenna number, niIndicate emptyWhite Gaussian noise on base i antenna, mean power are denoted as σ2
Step 4: ground base station uses the uniform linear array antenna of half-wave spacing, and each faces between null base station and carry outMillimeter wave beam communication obtains and respectively faces the channel response vector of null base station;
Ground base station and the channel response vector h for facing null base station iiFormula are as follows:
Wherein λi,lIndicate the complex coefficient of the l articles diameter of space base i, LiIndicate the multipath component total number for facing null base station i,Ωi,lIndicate the l articles diameter of space base i in the cosine value of the ground base station angle of departure, i.e. cos (AoD);A () indicates to be directed toward vectorFunction, expression formula are as follows:
A (N, Ω)=[ejπ0Ω,ejπ1Ω,ejπ2Ω,…,ejπ(N-1)Ω] (4)
A (N, Ω) depends on the geometry of array antenna;Use θi,lIndicate the angle of departure for facing the l articles diameter of null base station iValue, and Ωi,l=cos (θi,l)。
Step 5: selecting the channel response vector on most strong path as ground base station for each path for facing null base station iWith the efficient channel response vector h for facing null base station ii
hiia(N,Ωi) (5)
Wherein λiIndicate the complex coefficient in the most strong path of space base i, i.e., | λi|≥|λi,l|。
Step 6: using the wave beam forming vector w under permanent modular constraint, the efficient channel gain to null base station is respectively facedCorresponding sequence is made, the decoding priority orders of each space base signal are obtained.
Efficient channel gain depends on channel gain and array gain, and efficient channel gain is lower, and decoding priority is higher;
For | λ1| > | λ2|, i.e. the channel gain of space base 1(NOMA) is accessed according to non-orthogonal multipleCriterion, ground base station will carry out corresponding power distribution, the lower space base priority of channel gain according to the priority of space baseIt is higher;The signal that priority when the signal decoding of space base 2 is higher than space base 1 decodes priority;
For efficient channel gainPriority is higher than the signal solution of space base 2 when the signal decoding of space base 1Code priority;
Step 7: being ordered as efficient channel gainGround base station will emit signal s2Preferential solutionCode simultaneously eliminates in the signal of superposition, and further decoding emits signal s1, space base 2, which directly decodes, emits signal s2, obtain each space baseUp to rate;
It is eliminated from the signal of superposition using serial interference elimination method (SIC) by signal is emitted at space base end;Optimal solutionCode sequence is successively decoded from low to high according to channel gain, and in this order, each space base first decodes priorityHigh space base signal is deleted them in receiving signal, finally decodes the signal of oneself and no longer by the high (power of priorityIt is high) space base effect of signals.In this way, space base 1 can be deleted by serial interference and be avoided in space base NOMA system of the inventionThe influence of 2 signal of space base;The space base high as priority of space base 2 need not be deleted using serial interference.In brief, space base 1 is firstFirst decode s2, in its reception signal y1It is middle s2It deletes, then decodes s1;And space base 2 is s1Interference as noise processed, directlyDecode s2
The reachable rate of two space bases is calculated separately using shannon formula, as follows:
R1For the reachable rate of space base 1;R2For the reachable rate of space base 2;
Step 8: when all the sum of reachable rates for facing null base station reach maximization, the distribution of design joint Power and wave beamThe constraint condition that figuration need to meet.
Reach maximization i.e. objective function up to the sum of rate, as follows:
The above space base up to rate calculation formula obtain premise have it is assumed hereinafter that: space base 1 decode s2When Signal to Interference plus Noise Ratio(SINR) otherwise s is decoded lower than space base 22Signal to Interference plus Noise Ratio, otherwise will lead to space base 1 decode s2Rate be lower than space base 2, thenAccording to above-mentioned reachable rate calculation formula, space base 1 is in decoding s1Shi Wufa deletes s completely2Interference;This is claimed to be assumed to be implicit letterIt is dry to make an uproar than it is assumed that as follows:
To obtain reasonable power distribution and beam form-endowing method, the constraint condition that need to meet is as follows:
Wherein riIndicate the minimum reachable rate constraint for facing null base station i;P is the maximum power for facing the transmitting signal of null base station.
Step 9: solving to the constraint condition that need to meet, respectively faced the corresponding power distribution of null base station and ground base stationBeamforming scheme, obtain good performance.
Specific step is as follows:
First, by maximized each the sum of reachable rate for facing null base station, power control and beam gain distribution are split asSubproblem and wave beam forming two sub-problems, and introduce intermediate variableIt is converted.
Under ideal wave beam forming, beam gain meets:
Power control and beam gain distribution subproblem statement as a result, are as follows:
Reach maximization up to the sum of rate are as follows:
The condition that need to meet is as follows:
The statement of wave beam forming subproblem are as follows:
Wherein, α is the intermediate variable introduced, so that each component of wave beam forming vector approaches permanent modular constraint condition;[w]iIndicate i-th of element of w;
Then, to after conversion power control and beam gain distribution subproblem solve;
By to the problem objective function derivation, it can be found that objective function is p1Increasing function, and the reachable rate of space base 1It is p1Increasing function, the reachable rate of space base 2 is p1Subtraction function, then the reachable rate of space base 2 is necessarily etc. when the problem takes optimal solutionIt is minimum up to rate constraint in it, it may be assumed that
P as a result,1,p2,c2C can be used1It indicates, which becomes about c1Single argument optimization problem, can by derivationTo obtain its optimal solution are as follows:
Simultaneously, the wave beam forming subproblem after conversion is solved;
DefinitionWave beam forming formula (11) becomes:
Obviously, wave beam forming vector w can integrally carry out phase rotation, and not interfere with the value of beam gain,So if w is optimal solution,It is also optimal solution, whereinRepresent the amount of phase rotation, value range be [0,2 π).Do not lose oneAs property, suitable the amount of phase rotation is selected by phase rotationSo thatIt is real number, wave beam forming subproblem is converted are as follows:
Further decompose into the convex optimization problem of several standards, it can be seen that the last one constraint condition of formula (15)The sign of inequality left side is the ABS function of a linear function, and the right is a constant, is substantially to requireMould length be not less thanBecause not knowing that optimal solution is correspondingPhase, therefore cannot be equally simpleIt regards real number as, but passes through corresponding when search w acquirement optimal solutionPhase, giveMake its change multiplied by different phasesLinear constraint can always find the optimal solution of the problem as long as the phase of search is accurate enough;It finally obtains and formula (15)The convex optimization problem of a series of standard of equal value:
Wherein M is phase search total number, m=1,2..., M.Correspondence is searched for each time, it is clear that M is bigger, and search precision is got overHeight, obtained solution are more accurate;This M problem can be solved with the convex optimization tool of standard, and α in all optimization problems is selected to takeThat solution of minimum value is denoted asThen power normalization is carried out to wave beam forming vector
Finally, rightPermanent mould normalization is carried out, is keptThe phase invariant of each component uniformly becomes lengthTableIt is as follows up to formula:
In final power distribution and beamforming scheme as a result, respectively formula (13)In formula (17)W*

Claims (3)

Translated fromChinese
1.临空阵列通信非正交多址接入下行传输方法,其特征在于,具体步骤如下:1. a non-orthogonal multiple access downlink transmission method for air-space array communication, is characterized in that, concrete steps are as follows:步骤一、针对下行临空非正交多址接入通信系统,构建地面基站和临空基站之间的通信场景;Step 1, for the downlink airborne non-orthogonal multiple access communication system, construct a communication scenario between the ground base station and the airborne base station;通信场景包括:1.地面基站对多个临空基站的下行传输;2.临空基站对多个地面用户的下行传输;3.地面基站服务多个低空无人机的下行传输;The communication scenarios include: 1. Downlink transmission from the ground base station to multiple airborne base stations; 2. Downlink transmission from the airborne base station to multiple ground users; 3. The ground base station serves the downlink transmission of multiple low-altitude UAVs;步骤二、针对第一种场景模型,地面基站将对所有临空基站发送的功率归一化信号进行叠加发射;Step 2: For the first scenario model, the ground base station will superimpose and transmit the power normalized signals sent by all the airborne base stations;叠加信号表达式为:The superposition signal expression is:si表示地面基站给临空基站i发送的发射信号,pi为对临空基站i的发射信号功率;i=1,2;si represents the transmission signal sent by the ground base station to the airborne base stationi , and pi is the transmission signal power to the airborne base station i; i=1,2;步骤三、叠加信号s经过地面基站和临空基站之间的信道响应以及天线噪声后形成混合信号,并被两个临空基站各自接收;Step 3. The superimposed signal s forms a mixed signal after passing through the channel response between the ground base station and the airborne base station and the antenna noise, and is received by the two airborne base stations respectively;临空基站1接收的混合信号为:The mixed signal received by the airport base station 1 is:临空基站2接收的混合信号为:The mixed signal received by the airport base station 2 is:其中hi是地面基站和空基i的信道响应向量,w表示恒模约束下的波束赋形向量,其恒模约束为各分量模长相等N为地面基站天线个数,ni表示空基i天线上的高斯白噪声,其平均功率记为σ2where hi is the channel response vector of the ground base station and the space base i, w is the beamforming vector under the constant modulus constraint, and the constant modulus constraint is that the modulus lengths of each component are equal N is the number of ground base station antennas, ni is the Gaussian white noise on the space-based i antenna, and its average power is denoted as σ2 ;步骤四、地面基站采用半波间距的均匀线性阵列天线,和每个临空基站之间进行毫米波定向通信,得到与各临空基站的信道响应向量;Step 4: The ground base station adopts a uniform linear array antenna with half-wave spacing, and performs millimeter-wave directional communication with each airborne base station, and obtains a channel response vector with each airborne base station;地面基站和临空基站i的信道响应向量hi公式为:The formula of the channel response vector hi of the ground base station and the airborne base station i is:其中λi,l表示空基i的第l条径的复系数,Li表示临空基站i的多径分量总个数,Ωi,l表示空基i的第l条径在地面基站发射角的余弦值,a(·)表示指向向量的函数,其表达式为:where λi,l represents the complex coefficient of the lth path of the space base i, Li represents the total number of multipath components of the airborne base station i, and Ωi,l represents the lth path of the space base i transmitted by the ground base station The cosine value of the angle, a( ) represents the function of the pointing vector, and its expression is:a(N,Ω)=[ejπ0Ω,ejπ1Ω,ejπ2Ω,…,ejπ(N-1)Ω]a(N,Ω)=[ejπ0Ω ,ejπ1Ω ,ejπ2Ω ,…,e jπ(N-1)Ω ]a(N,Ω)取决于阵列天线的几何结构;a(N,Ω) depends on the geometry of the array antenna;步骤五、针对临空基站i的各路径,选择最强路径上的信道响应向量作为地面基站与临空基站i的有效信道响应向量hiStep 5, for each path of the airborne base station i, select the channel response vector on the strongest path as the effective channel response vector hi of the ground base station and the airborne base station i ;hi=λia(N,Ωi)hii a(N,Ωi )其中λi表示空基i的最强路径的复系数,即|λi|≥|λi,l|;where λi represents the complex coefficient of the strongest path of the space base i, ie |λi |≥|λi,l |;步骤六、利用恒模约束下的波束赋形向量w,对各临空基站的有效信道增益做出相应排序,得到各空基信号的解码优先级顺序;Step 6: Use the beamforming vector w under the constant modulus constraint to obtain the effective channel gain of each airborne base station Make corresponding sorting to obtain the decoding priority order of each space-based signal;有效信道增益取决于信道增益和阵列增益,有效信道增益越低,解码优先级越高;The effective channel gain depends on the channel gain and array gain, the lower the effective channel gain, the higher the decoding priority;针对有效信道增益空基2的信号解码时的优先级高于空基1的信号解码优先级;For effective channel gain The decoding priority of the space-based 2 signal is higher than the decoding priority of the space-based 1 signal;针对有效信道增益空基1的信号解码时的优先级高于空基2的信号解码优先级;For effective channel gain The priority of the signal decoding of the space base 1 is higher than that of the signal decoding of the space base 2;步骤七、针对有效信道增益排序为空基1将发射信号s2优先解码并在叠加的信号中消除掉,再解码发射信号s1,空基2直接解码发射信号s2,得到各空基的可达率;采用香农公式分别计算两个空基的可达率,如下:Step 7. The effective channel gain is sorted as The space base 1 decodes the transmitted signal s2 preferentially and eliminates it in the superimposed signal, and then decodes the transmitted signal s1 , and the space base 2 directly decodes the transmitted signal s2 to obtain the reachability of each space base; use Shannon formula to calculate respectively The reachability of the two empty bases is as follows:空基1的可达率R1为:The reachability ratio R1 of space base 1 is:空基2的可达率R2为:The reachability R2 of space base 2 is:步骤八、当所有临空基站的可达率之和达到最大化时,设计联合功率分配及波束赋形需满足的约束条件;Step 8. When the sum of the reachability rates of all airborne base stations is maximized, design the constraints that must be met by joint power allocation and beamforming;可达率之和达到最大化也就是目标函数,如下:The sum of the reachability rates is maximized, which is the objective function, as follows:需满足的约束条件如下:The constraints to be satisfied are as follows:p1+p2=Pp1 +p2 =P其中ri表示临空基站i的最低可达率约束;P为临空基站的发射信号的最大功率;where ri represents the minimum reachability constraint of the airport base stationi ; P is the maximum power of the transmitted signal of the airport base station;步骤九、对需满足的约束条件求解,得到各临空基站相应的功率分配和地面基站的波束赋形方案,取得良好的性能。Step 9: Solve the constraints that need to be satisfied, obtain the corresponding power allocation of each airborne base station and the beamforming scheme of the ground base station, and obtain good performance.2.如权利要求1所述的临空阵列通信非正交多址接入下行传输方法,其特征在于,所述的步骤一中,第一种地面基站对多个临空基站的下行传输的场景,具体构建如下:2. The non-orthogonal multiple access downlink transmission method for airborne array communication according to claim 1, characterized in that, in the step 1, the first ground base station performs the downlink transmission of multiple airborne base stations. The scenario is constructed as follows:地面基站有N元天线阵列,在同一时域/频域/码域资源块内连接2个单天线远程临空基站,两个临空基站分别为空基1和空基2;在地面基站一端,每根天线分支有一个相位转换器和功率放大器,所有的功率放大器有相同的比例因子,因此波束赋形向量,即天线权系数向量每一个分量的模长相等,称之为恒模约束。The ground base station has an N-element antenna array, and two single-antenna remote airborne base stations are connected in the same time domain/frequency domain/code domain resource block, and the two airborne base stations are space base 1 and space base 2 respectively; , each antenna branch has a phase converter and a power amplifier, and all power amplifiers have the same scale factor, so the beamforming vector, that is, the antenna weight coefficient vector, each component has the same modulus length, which is called constant modulus constraint.3.如权利要求1所述的临空阵列通信非正交多址接入下行传输方法,其特征在于,所述的步骤九具体步骤如下:3. The non-orthogonal multiple access downlink transmission method for air array communication as claimed in claim 1, is characterized in that, the concrete steps of described step 9 are as follows:首先、将最大化的各个临空基站的可达率之和,拆分为功率控制及波束增益分配子问题和波束赋形两个子问题,并引入中间变量进行转换;First, divide the maximized sum of the reachability of each airport base station into two sub-problems of power control and beam gain allocation and beam forming, and introduce intermediate variables convert;在理想波束赋形下,波束增益满足:Under ideal beamforming, the beam gain satisfies:由此,功率控制及波束增益分配子问题表述为:Therefore, the power control and beam gain allocation subproblems are formulated as:可达率之和达到最大化为:The sum of the reachability rates is maximized as:需满足的条件如下:The conditions to be met are as follows:p1+p2=Pp1 +p2 =P波束赋形子问题表述为:The beamforming subproblem is formulated as:其中,α为引入的中间变量,使得波束赋形向量各个分量逼近恒模约束条件;[w]i表示w的第i个元素;Among them, α is an intermediate variable introduced, so that each component of the beamforming vector approximates the constant modulus constraint; [w]i represents the ith element of w;然后、对转换后的功率控制及波束增益分配子问题进行求解;Then, the converted power control and beam gain allocation sub-problems are solved;该问题求得最优解时空基2的可达率等于其最小可达率约束,即For this problem, the reachability of the optimal solution space-time basis 2 is equal to its minimum reachability constraint, that is,通过求导得到功率控制及波束增益分配子问题的最优解为:The optimal solution of the power control and beam gain allocation sub-problems is obtained by derivation as:同时、对转换后的波束赋形子问题进行求解;At the same time, the transformed beamforming sub-problem is solved;定义波束赋形子问题变为:definition The beamforming subproblem becomes:通过相位旋转选择合适的相位旋转量使得是实数,将波束赋形子问题转化为:Select the appropriate amount of phase rotation through phase rotation make is a real number, transforming the beamforming subproblem into:进一步分解成若干标准凸优化问题,通过搜索w取得最优解时相应的的相位,给乘以不同的相位使其变成线性约束,得到等价的一系列的标准凸优化问题:It is further decomposed into several standard convex optimization problems, and when the optimal solution is obtained by searching w, the corresponding phase, giving Multiplying by different phases to make it a linear constraint yields an equivalent series of standard convex optimization problems:其中M为相位搜索总个数,m=1,2...,M;where M is the total number of phase searches, m=1,2...,M;用标准的凸优化工具求解,选择所有优化问题中α取最小值的那个解记为然后对波束赋形向量进行功率归一化Use standard convex optimization tools to solve, select the solution with the minimum value of α in all optimization problems and record it as The beamforming vector is then power normalized最后,对进行恒模归一化,保持各分量的相位不变,把长度统一变为表达式如下:Finally, yes Perform constant modulus normalization, keep The phase of each component is unchanged, and the length is unified into The expression is as follows:由此,最终的功率分配和波束赋形方案,分别为和w*Thus, the final power allocation and beamforming schemes, respectively, are and w* .
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