CN110943752A - An OQPSK Adaptive Variable Rate Digital Transceiver Based on Proximity Space Link Protocol - Google Patents
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Abstract
本发明公开了一种基于邻近空间链路协议的OQPSK系统自适应变速率数字收发机。发射机包括OQPSK调制模块和发射机速率控制模块,接收机包括OQPSK解调模块、信噪比估计模块和接收机速率控制模块;发射机根据接收机反馈信息对发射机的参数配置进行调整,通过发射机速率控制模块控制时钟模块、内插倍数、抽取倍数调整发射信号速率。接收机通过信噪比估计模块对接收到的信号进行信噪比估计,接收机速率控制模块根据信噪比估计值控制接收机的钟模块、内插倍数、抽取倍数,同时向发射机提供速率反馈信息,同步进行自适应速率切换。此数字收发机能有效面对深空通信信道恶劣的环境。
The invention discloses an OQPSK system adaptive variable rate digital transceiver based on the adjacent space link protocol. The transmitter includes an OQPSK modulation module and a transmitter rate control module, and the receiver includes an OQPSK demodulation module, a signal-to-noise ratio estimation module and a receiver rate control module; the transmitter adjusts the parameter configuration of the transmitter according to the feedback information of the receiver, through The transmitter rate control module controls the clock module, the interpolation multiple, and the decimation multiple to adjust the transmission signal rate. The receiver estimates the signal-to-noise ratio of the received signal through the signal-to-noise ratio estimation module, and the receiver rate control module controls the receiver's clock module, interpolation multiple, and extraction multiple according to the estimated signal-to-noise ratio, and provides the transmitter with the rate. Feedback information, synchronously perform adaptive rate switching. This digital transceiver can effectively face the harsh environment of deep space communication channels.
Description
技术领域:Technical field:
本发明涉及深空环境中损耗差异较大背景下用于近邻链路空间的自适应数字收发机设计,尤其是一种基于邻近空间链路协议的OQPSK自适应变速率数字收发机。The invention relates to the design of an adaptive digital transceiver for adjacent link space under the background of large loss difference in a deep space environment, in particular to an OQPSK adaptive variable rate digital transceiver based on the adjacent space link protocol.
背景技术:Background technique:
美国航天局(NASA)、欧洲航天局(ESA)等多过航天机构于上世纪80年代创立了国际空间数据系统咨询委员会(Consultative Committee for Space Data Systems,CCSDS),针对深空通信特点,提高深空信道资源的利用率,为实现国际间深空探侧的紧密合作,提出了CCSDS标准协议,也就是邻近空间链路协议。根据CCSDS Proximity-1协议标准,对航天器与航天器、航天器与地面、航天器与着陆器之前的通信进行了规范,该标准要求深空收发机支持1kbps、2kpbs、4kbps、8kbps~1024kbps、2048kbps范围中12档传输速率的切换,并满足链路余量应为异步链路提供小于10-6的误码率。More than space agencies such as NASA and the European Space Agency (ESA) established the Consultative Committee for Space Data Systems (CCSDS) in the 1980s. The utilization rate of space channel resources, in order to realize the close cooperation of the international deep space exploration side, proposed the CCSDS standard protocol, that is, the adjacent space link protocol. According to the CCSDS Proximity-1 protocol standard, the communication between the spacecraft and the spacecraft, the spacecraft and the ground, and the spacecraft and the lander is standardized. Switching of 12 transmission rates in the range of 2048kbps and meeting the link margin should provide a bit error rate of less than 10 -6 for the asynchronous link.
相比于地面传统通信,深空信道的恶变程度要剧烈很多,图2所示即为深空信道衰减模型,发射信号往往不仅要受到多普勒频移、多径延迟等小尺度衰落影响,而且会受到路径损耗、宇宙噪声、行星噪声、太阳闪烁等大尺度衰落影响,从而会造成信道容量的急剧变化。因此,固定传输速率的通信无法满足深空信道的需求。Compared with the traditional communication on the ground, the deterioration degree of the deep space channel is much more severe. Figure 2 shows the deep space channel attenuation model. The transmitted signal is often not only affected by small-scale fading such as Doppler frequency shift and multipath delay. In addition, it will be affected by large-scale fading such as path loss, cosmic noise, planetary noise, and solar scintillation, resulting in a sharp change in channel capacity. Therefore, fixed transmission rate communication cannot meet the needs of deep space channels.
发明内容:Invention content:
发明目的:为了解决深空通信恶劣信道条件对信号传输的有效性和可靠性的影响,本发明结合邻近空间链路协议,提出了基于邻近空间链路协议的OQPSK自适应变速率数字收发机,通过信噪比估计模块输出信息控制收发机的自适应速率控制模块,得到当前误码率要求下所需的码元速率,之后自适应控制模块控制收发机时钟模块,改变内插抽取倍数,同时控制收发机滤波器带宽,保证在满足误码率的前提下尽可能的提高信号的吞吐量,满足深空通信的收发机通过自适应变速率技术来降低信道变化对收发机产生的影响的需求,提高信号传输的实时性与有效性。Purpose of the invention: In order to solve the influence of the bad channel conditions of deep space communication on the validity and reliability of signal transmission, the present invention combines the adjacent space link protocol, and proposes an OQPSK adaptive variable rate digital transceiver based on the adjacent space link protocol. The adaptive rate control module of the transceiver is controlled by the output information of the signal-to-noise ratio estimation module to obtain the required symbol rate under the current bit error rate requirement, and then the adaptive control module controls the transceiver clock module to change the interpolation and extraction multiples, and at the same time Control the bandwidth of the transceiver filter to ensure that the signal throughput can be improved as much as possible on the premise of satisfying the bit error rate, and meet the needs of the deep space communication transceiver to reduce the impact of channel changes on the transceiver through adaptive variable rate technology. , to improve the real-time and effectiveness of signal transmission.
发明内容:为实现上述技术效果,本发明提出一种基于邻近空间链路协议的OQPSK自适应变速率数字收发机,包括发射机和接收机;其中,SUMMARY OF THE INVENTION: In order to achieve the above technical effects, the present invention proposes an OQPSK adaptive variable rate digital transceiver based on the adjacent space link protocol, including a transmitter and a receiver; wherein,
发射机包括OQPSK调制模块和发射机速率控制模块;The transmitter includes an OQPSK modulation module and a transmitter rate control module;
接收机包括OQPSK解调模块、信噪比估计模块和接收机速率控制模块;The receiver includes an OQPSK demodulation module, a signal-to-noise ratio estimation module and a receiver rate control module;
接收机接收发射机发送的信号,通过OQPSK解调模块解调后送至信噪比估计模块,信噪比估计模块对接收到的信号进行信噪比估计,并将估计值发送给接收机速率控制模块;接收机速率控制模块接收上位机发来的误码率要求,计算出所需信噪比大小,再与信噪比估计模块的估计出的信噪比比较,利用OQPSK信号降低一半符号速率信噪比提升3dB和OQPSK信号升高一倍符号速率信噪比降低3dB的特点,通过对时钟模块、内插抽取倍数的调整改变码元速率,使信号速率进行逐级调整,直至信噪比达到所需信噪比要求,然后将调整后达到所需信噪比要求的信号速率反馈给发射机速率控制模块;The receiver receives the signal sent by the transmitter, demodulates it through the OQPSK demodulation module, and then sends it to the SNR estimation module. The SNR estimation module estimates the SNR of the received signal, and sends the estimated value to the receiver. Control module; the receiver rate control module receives the bit error rate request sent by the host computer, calculates the required SNR, and then compares it with the estimated SNR from the SNR estimation module, and uses the OQPSK signal to reduce the symbol by half The rate signal-to-noise ratio is increased by 3dB and the OQPSK signal is doubled. The symbol rate is reduced by 3dB. The symbol rate is changed by adjusting the clock module and the interpolation and extraction multiples, so that the signal rate is adjusted step by step until the signal-to-noise ratio is adjusted. ratio to meet the required signal-to-noise ratio requirements, and then feedback the adjusted signal rate to meet the required signal-to-noise ratio requirements to the transmitter rate control module;
发射机速率控制模块接收接收机发来的信号速率反馈信息,根据接收机速率反馈信息调整发射机的时钟模块、内插倍数、抽取倍数,改变发射机的发射速率至所需发射速率;同时,将发射机新的速率信息与发射机相关参数信息写入SPDU中,随着邻近链路传输单元发送给接收机。The transmitter rate control module receives the signal rate feedback information sent by the receiver, adjusts the transmitter's clock module, interpolation multiple and decimation multiple according to the receiver rate feedback information, and changes the transmitter's transmission rate to the desired transmission rate; at the same time, Write the transmitter's new rate information and transmitter-related parameter information into the SPDU, and send it to the receiver along with the adjacent link transmission unit.
进一步的,所述接收机的OQPSK解调模块包括依次级联的数字下变频模块、增益检测模块、自动增益控制模块、载波同步模块、符号同步模块、帧同步模块、相位补偿与判决模块和串并转换模块;其中,Further, the OQPSK demodulation module of the receiver includes a digital down-conversion module, a gain detection module, an automatic gain control module, a carrier synchronization module, a symbol synchronization module, a frame synchronization module, a phase compensation and judgment module, and a serial and transform the module; where,
数字下变频模块将接收机接收到的信号转换为们所需的低中频信号;The digital down-conversion module converts the signal received by the receiver into the required low-IF signal;
增益检测模块对接收信号进行能量检测,当接收信号的能量高于预设的能量检测门限值时,判断接收信号属于有用用户信息,此时接收机开启;当接收信号的能量低于预设的能量检测门限值时,判断接收信号属于无效噪声,此时接收机关闭;The gain detection module performs energy detection on the received signal. When the energy of the received signal is higher than the preset energy detection threshold, it is judged that the received signal belongs to useful user information, and the receiver is turned on at this time; when the energy of the received signal is lower than the preset energy detection threshold When the energy detection threshold value is higher than the energy detection threshold, it is judged that the received signal is invalid noise, and the receiver is turned off at this time;
自动增益控制模块在接收机接收信号由于信道衰落、宇宙噪音产生较大幅度的振荡时对增益系数进行自适应调整,防止信号饱和或丢失,使接收信号满足后级同步解调要求;The automatic gain control module adjusts the gain coefficient adaptively when the received signal of the receiver oscillates with a relatively large amplitude due to channel fading and cosmic noise, to prevent signal saturation or loss, and to make the received signal meet the requirements of post-stage synchronous demodulation;
载波同步模块通过对接收信号进行闭环检测,动态的调整接收机本地载波的频率,使其与发射机载波频率相等,使接收机后续模块可以进行相干解调;The carrier synchronization module dynamically adjusts the frequency of the local carrier of the receiver to make it equal to the carrier frequency of the transmitter through closed-loop detection of the received signal, so that the subsequent modules of the receiver can perform coherent demodulation;
符号同步模块和帧同步模块分别对接收到的信号进行符号同步和帧同步处理;The symbol synchronization module and the frame synchronization module respectively perform symbol synchronization and frame synchronization processing on the received signal;
相位补偿与判决模块通过对相位偏差的估计进行补偿,之后进行判决得到用户比特信息;The phase compensation and judgment module compensates by estimating the phase deviation, and then judges to obtain user bit information;
串并转换模块将相位补偿与判决模块输出的信号进行串并转换后输出用户信息。The serial-to-parallel conversion module performs serial-to-parallel conversion on the signal output by the phase compensation and decision module, and then outputs the user information.
进一步的,所述自动增益控制模块包括可控增益放大器、检测器模块、增益系数控制模块、比较器、误差处理模块;Further, the automatic gain control module includes a controllable gain amplifier, a detector module, a gain coefficient control module, a comparator, and an error processing module;
输入信号在经过A/D转换与可控增益放大器后进入检测器,检测器对信号能量进行检测,并将检测结果分别送入比较器和增益系数控制模块;The input signal enters the detector after A/D conversion and controllable gain amplifier, the detector detects the signal energy, and sends the detection results to the comparator and the gain coefficient control module respectively;
比较器将接收到的检测值与基准值进行比较,得到与基准值的误差后将误差值送入误差处理模块;The comparator compares the received detection value with the reference value, and sends the error value to the error processing module after obtaining the error with the reference value;
增益系数控制模块根据检测值对误差处理模块中的增益系数进行调整;其调整公式为Gain(n+1)=Gain(n)+aVe,其中,Gain(n+1)为调整后的增益系数,Gain(n)为当前增益系数,a为加权因子,Ve为与标准值误差;The gain coefficient control module adjusts the gain coefficient in the error processing module according to the detected value; the adjustment formula is Gain(n+1)=Gain(n)+aV e , where Gain(n+1) is the adjusted gain coefficient, Gain(n) is the current gain coefficient, a is the weighting factor, and V e is the error from the standard value;
误差处理模块根据接收到的误差值和增益系数调整结果,对可控增益放大器的增益系数进行调整:当误差值低于阈值时,可控增益放大器的增益系数保持不变,当误差值超过阈值时,增益系数根据误差处理模块反馈信息进行改变,得到新的可控增益放大器放大系数。The error processing module adjusts the gain coefficient of the controllable gain amplifier according to the received error value and the gain coefficient adjustment result: when the error value is lower than the threshold value, the gain coefficient of the controllable gain amplifier remains unchanged, and when the error value exceeds the threshold value When , the gain coefficient is changed according to the feedback information of the error processing module to obtain a new controllable gain amplifier amplification coefficient.
进一步的,所述载波同步模块采用修正Costas环来实现,所述修正Costas环包括本地NCO、匹配滤波器、数字鉴相器、环路滤波器;接收机接收到的I路、Q路信号经过匹配滤波器后进入数字鉴相器,所得到的鉴相器输出信号在经过环路滤波器后对接收机的本地NCO进行调整,直到接收机本地NCO与接收信号载波频率相一致后环路达到稳定。Further, the carrier synchronization module is implemented by using a modified Costas loop, and the modified Costas loop includes a local NCO, a matched filter, a digital phase detector, and a loop filter; After the matched filter enters the digital phase detector, the obtained output signal of the phase detector adjusts the local NCO of the receiver after passing through the loop filter, until the local NCO of the receiver is consistent with the carrier frequency of the received signal, the loop reaches Stablize.
进一步的,所述符号同步模块采用迟早环算法进行符号同步设计,包括:早门积分器、迟门积分器、数据误差鉴别器、环路滤波器、锁定判决器与时钟发生器;对I路、Q路信号进行归一化处理,处理后所得方波信号分别进入早门积分器与迟门积分器,I路信号的早、迟门积分结果和Q路信号的早、迟门积分结果送入数据误差鉴别器进行判决,当存在时钟误差时,数据误差鉴别器会迅速累积误差并给出误差数据,误差数据在经过环路滤波器后对时钟发生器进行调整,改变早门时钟、迟门时钟和采样时钟的时钟频率,直到得到最佳采样时刻,同时,锁定判决器会给出锁定指示,清楚的反应符号同步模块的工作状态。Further, the symbol synchronization module adopts an early and early loop algorithm to carry out symbol synchronization design, including: an early gate integrator, a late gate integrator, a data error discriminator, a loop filter, a lock decision device and a clock generator; , Q channel signals are normalized, the square wave signal obtained after processing enters the early gate integrator and the late gate integrator respectively, the early and late gate integration results of the I channel signal and the early and late gate integration results of the Q channel signal are sent to When there is a clock error, the data error discriminator will quickly accumulate the error and give the error data. After the error data passes through the loop filter, the clock generator is adjusted to change the early gate clock, late gate clock and late gate clock. The clock frequency of the gate clock and the sampling clock is determined until the optimal sampling time is obtained. At the same time, the lock decision device will give a lock indication to clearly reflect the working status of the symbol synchronization module.
进一步的,所述信噪比估计模块包括信噪比估计算法选择模块、DF-3估计算法模块、SNV估计算法模块和信噪比输出模块,所述DF-3估计算法模块采用DF-3估计算法由输入信号计算得到信噪比估计值,SNV估计算法模块采用SNV估计算法由输入信号计算得到信噪比估计值;信噪比输出模块将上一时刻信噪比估计值作为信噪比反馈信息输入信噪比估计算法选择模块,信噪比估计模块通过对比信噪比反馈信息与模块内所设定的门限值进行后级估计模块的选择:当信噪比发生变化超过门限值时,信噪比估计算法会在下一时刻进行切换。Further, the signal-to-noise ratio estimation module includes a signal-to-noise ratio estimation algorithm selection module, a DF-3 estimation algorithm module, an SNV estimation algorithm module and a signal-to-noise ratio output module, and the DF-3 estimation algorithm module adopts DF-3 estimation. The algorithm calculates the SNR estimate from the input signal, and the SNV estimation algorithm module uses the SNV estimation algorithm to calculate the SNR estimate from the input signal; the SNR output module feeds back the SNR estimate at the previous moment as the SNR The information is input to the signal-to-noise ratio estimation algorithm selection module, and the signal-to-noise ratio estimation module selects the subsequent estimation module by comparing the signal-to-noise ratio feedback information with the threshold value set in the module: when the signal-to-noise ratio changes beyond the threshold value , the SNR estimation algorithm will switch at the next moment.
有益效果:本发明具有如下优势:Beneficial effects: the present invention has the following advantages:
1.根据邻近空间链路协议要求,该数字收发机支持1kbps、2kpbs、4kbps、8kbps~1024kbps、2048kbps范围中12档传输速率的切换。1. According to the requirements of the adjacent space link protocol, the digital transceiver supports the switching of 12 transmission rates in the range of 1kbps, 2kpbs, 4kbps, 8kbps ~ 1024kbps, and 2048kbps.
2.相比于QPSK调制系统,本系统采用OQPSK调制方式,避免了180°的相位翻转,提高了相位补偿与判决性能,减少由相位偏差产生的误码。2. Compared with the QPSK modulation system, the system adopts the OQPSK modulation method, which avoids the 180° phase inversion, improves the phase compensation and decision performance, and reduces the bit error caused by the phase deviation.
3.接收机增益检测模块由上位机设置工作状态,调整检测门限值,满足不同环境下的工作需求。3. The receiver gain detection module is set by the host computer to set the working state and adjust the detection threshold to meet the work requirements in different environments.
4.自动增益控制模块采用可变增益系数,减少反馈环路的稳定时间,有效地解决信号衰落较大的问题。4. The automatic gain control module adopts variable gain coefficient to reduce the stabilization time of the feedback loop and effectively solve the problem of large signal fading.
5.信噪比估计模块采用DF-3估计与SNV估计联合估计的方法,结合两种估计算法的优势,达到硬件复杂度较低,信噪比估计误差小的效果,有效解决了深空通信信道时变性大的问题。5. The signal-to-noise ratio estimation module adopts the joint estimation method of DF-3 estimation and SNV estimation, and combines the advantages of the two estimation algorithms to achieve the effect of low hardware complexity and small signal-to-noise ratio estimation error, effectively solving deep space communication. The problem of large time-varying channel.
6.采用自适应变速率设计,可以根据上位机设置误码率要求,并根据当前信道质量与当前数据速率进行自适应变速率调整,通过对时钟模块、内插抽取倍数的调整,改变收发机的数据速率,在满足信噪比要求的前提下提高信息吞吐量,满足不同背景下的深空通信要求。6. Adopting the adaptive variable rate design, the bit error rate requirements can be set according to the host computer, and the adaptive variable rate can be adjusted according to the current channel quality and current data rate, and the transceiver can be changed by adjusting the clock module and the interpolation and extraction multiples. It can improve the information throughput under the premise of meeting the requirements of signal-to-noise ratio, and meet the requirements of deep space communication in different backgrounds.
附图说明:Description of drawings:
图1为实施例所述数字收发机的结构图;Fig. 1 is the structure diagram of the digital transceiver according to the embodiment;
图2为深空信道衰减模型;Figure 2 is a deep space channel attenuation model;
图3为自动增益模块设计;Figure 3 is the automatic gain module design;
图4为修正Costas环符号同步设计;Figure 4 is a modified Costas ring symbol synchronization design;
图5为早迟环符号同步设计;Fig. 5 is the early and late ring symbol synchronization design;
图6为DF-3、SNV信噪比联合估计算法设计;Figure 6 shows the design of the joint estimation algorithm of DF-3 and SNV signal-to-noise ratio;
图7为OQPSK信号误码率曲线;Fig. 7 is the OQPSK signal bit error rate curve;
图8为误码率要求10-7,初始信噪比28dB,初始数据速率512kbps自适应变速率仿真图。Fig. 8 is a simulation diagram of a bit error rate requirement of 10 -7 , an initial signal-to-noise ratio of 28dB, and an initial data rate of 512kbps adaptive variable rate.
具体实施方式Detailed ways
本发明旨在提出一种能够解决深空通信恶劣信道条件对信号传输的有效性和可靠性的影响的数字收发机,该收发机结合了邻近空间链路协议,设计能够自适应变速率传输的数字收发机,可以有效地满足深空信道的传输要求,在满足误码率要求的前提下,尽可能的提高传输速率,在面对误码率更低的传输要求时,也极易对收发机的参数进行调整。The present invention aims to propose a digital transceiver that can solve the effect of bad channel conditions of deep space communication on the validity and reliability of signal transmission. Digital transceivers can effectively meet the transmission requirements of deep space channels. On the premise of meeting the requirements of the bit error rate, the transmission rate should be increased as much as possible. In the face of transmission requirements with a lower bit error rate, it is also easy to transmit and receive. machine parameters to adjust.
深空信道受多种因素影响,信号衰落变化幅度较大,主要衰落因素包括多普勒频移与多径损耗在内的小尺度衰落与包括路径损耗、太阳闪烁、宇宙噪声在内的大尺度衰落,信道容量变化较大。因此,传统固定速率通信无法满足深空信道要求,本文所设计的自适应收发机可以实时根据信道状况进行速率切换,满足通信要求。The deep space channel is affected by many factors, and the signal fading varies greatly. The main fading factors include small-scale fading including Doppler frequency shift and multipath loss and large-scale fading including path loss, solar scintillation, and cosmic noise. Fading, the channel capacity changes greatly. Therefore, the traditional fixed rate communication cannot meet the requirements of deep space channels. The adaptive transceiver designed in this paper can perform rate switching according to the channel conditions in real time to meet the communication requirements.
CCSDS Proximity-1协议对深空通信收发机的误码率进行了规定,而OQSPK调制解调系统的误码率会随着信噪比的提高而减小,所以在深空通信链路中,需要通过改变信号码元速率有效控制信噪比,从而满足协议收发机的传输需求。当码元速率降低时,信号带宽也会随之相应变窄,收发机所需滤波器带宽也会随之降低,滤波器所接收的带内噪声也会随之减小,在相同发射机发射功率下,信号功率不变,噪声功率减小,信噪比也就随之增高。反之,当信道条件良好时,可以通过提高码元速率,提高信号的吞吐量。The CCSDS Proximity-1 protocol specifies the bit error rate of the deep space communication transceiver, and the bit error rate of the OQSPK modulation and demodulation system will decrease with the increase of the signal-to-noise ratio, so in the deep space communication link, It is necessary to effectively control the signal-to-noise ratio by changing the signal symbol rate, so as to meet the transmission requirements of the protocol transceiver. When the symbol rate decreases, the signal bandwidth will also be narrowed accordingly, the filter bandwidth required by the transceiver will also decrease, and the in-band noise received by the filter will also decrease. Under the power, the signal power remains unchanged, the noise power decreases, and the signal-to-noise ratio increases accordingly. Conversely, when the channel conditions are good, the signal throughput can be improved by increasing the symbol rate.
变速率方式可以通过改变码元速率、改变调制方式、改变编码方式来实现,根据协议相关需求,可以采用改变码元速率的方式来实现自适应变速率设计,满足协议对于12种不同速率信号的要求。而采用改变码元速率的方式来进行变速率设计,由于不改变调制方式,且自适应数字收发机调制解调模块相对固定,因此只需要自适应控制模块控制收发机的时钟模块,内插抽取系数,满足收发机在不同速率下的调制解调要求即可。The variable rate method can be realized by changing the symbol rate, the modulation method, and the coding method. According to the relevant requirements of the protocol, the adaptive variable rate design can be realized by changing the symbol rate to meet the requirements of the protocol for 12 different rate signals. Require. However, the variable rate design is carried out by changing the symbol rate. Since the modulation method is not changed, and the modulation and demodulation module of the adaptive digital transceiver is relatively fixed, only the adaptive control module is required to control the clock module of the transceiver, and the interpolation and extraction The coefficients are sufficient to meet the modulation and demodulation requirements of the transceiver at different rates.
基于上述分析,本发明提出一种基于邻近空间链路协议的OQPSK自适应变速率数字收发机,包括发射机和接收机;其中,Based on the above analysis, the present invention proposes an OQPSK adaptive variable rate digital transceiver based on the adjacent space link protocol, including a transmitter and a receiver; wherein,
发射机包括OQPSK调制模块和发射机速率控制模块;The transmitter includes an OQPSK modulation module and a transmitter rate control module;
接收机包括OQPSK解调模块、信噪比估计模块和接收机速率控制模块;The receiver includes an OQPSK demodulation module, a signal-to-noise ratio estimation module and a receiver rate control module;
接收机接收发射机发送的信号,通过OQPSK解调模块解调后送至信噪比估计模块,信噪比估计模块对接收到的信号进行信噪比估计,并将估计值发送给接收机速率控制模块;接收机速率控制模块接收上位机发来的误码率要求,计算出所需信噪比大小,再与信噪比估计模块的估计出的信噪比比较,利用OQPSK信号降低一半符号速率信噪比提升3dB和OQPSK信号升高一倍符号速率信噪比降低3dB的特点,通过对时钟模块、内插抽取倍数的调整改变码元速率,使信号速率进行逐级调整,直至信噪比达到所需信噪比要求,然后将调整后达到所需信噪比要求的信号速率反馈给发射机速率控制模块;The receiver receives the signal sent by the transmitter, demodulates it through the OQPSK demodulation module, and then sends it to the SNR estimation module. The SNR estimation module estimates the SNR of the received signal, and sends the estimated value to the receiver. Control module; the receiver rate control module receives the bit error rate request sent by the host computer, calculates the required SNR, and then compares it with the estimated SNR from the SNR estimation module, and uses the OQPSK signal to reduce the symbol by half The rate signal-to-noise ratio is increased by 3dB and the OQPSK signal is doubled. The symbol rate is reduced by 3dB. The symbol rate is changed by adjusting the clock module and the interpolation and extraction multiples, so that the signal rate is adjusted step by step until the signal-to-noise ratio is adjusted. ratio to meet the required signal-to-noise ratio requirements, and then feedback the adjusted signal rate to meet the required signal-to-noise ratio requirements to the transmitter rate control module;
发射机速率控制模块接收接收机发来的信号速率反馈信息,根据接收机速率反馈信息调整发射机的时钟模块、内插倍数、抽取倍数,改变发射机的发射速率至所需发射速率;同时,将发射机新的速率信息与发射机相关参数信息写入SPDU中,随着邻近链路传输单元发送给接收机。The transmitter rate control module receives the signal rate feedback information sent by the receiver, adjusts the transmitter's clock module, interpolation multiple and decimation multiple according to the receiver rate feedback information, and changes the transmitter's transmission rate to the desired transmission rate; at the same time, Write the transmitter's new rate information and transmitter-related parameter information into the SPDU, and send it to the receiver along with the adjacent link transmission unit.
上述收发机采用OQPSK调制解调方式,由于I路、Q路信号存在Ts/2的延时,不会同时发生两路码元极性翻转,相较于传统的QPSK信号不会产生180°的相位误差,有助于接收机相位补偿与判决。同时OQPSK调制在通过带通滤波器后包络起伏小,性能较为稳定,频带较宽,有利于不同码速率之前的切换。The above transceiver adopts OQPSK modulation and demodulation method. Due to the delay of Ts/2 in the I channel and Q channel signals, the polarity of the two channels will not be reversed at the same time. Compared with the traditional QPSK signal, there will be no 180° deviation. The phase error is helpful for receiver phase compensation and judgment. At the same time, the envelope fluctuation of OQPSK modulation is small after passing through the band-pass filter, the performance is relatively stable, and the frequency band is wide, which is beneficial to the switching before different code rates.
下面结合附图通过具体实施例进一步阐述本发明的技术方案。The technical solutions of the present invention are further described below with reference to the accompanying drawings through specific embodiments.
图1所示是本发明所述收发机的一种实现方式:Figure 1 shows an implementation of the transceiver according to the present invention:
包括深空通信OQPSK自适应变速率发射机以及深空通信OQPSK自适应接收机;Including deep space communication OQPSK adaptive variable rate transmitter and deep space communication OQPSK adaptive receiver;
发射机采用OQPSK调制技术,在Q路信号加入半个码元周期延时,使I路、Q路信号不会同时发生极性翻转,产生180°的相位翻转,发射信号先进行串并转换得到I路、Q路信号,再通过插零、成型滤波、低通滤波等调制模块后与本地发射机NCO相乘后相加得到调制好的OQPSK信号,信号在经过数字上变频后进入深空信道。发射机具有发射机速率控制模块,可以接收接收机发来的速率反馈信息。通过接收机速率反馈信息改变发射机的发射速率,同时,将发射机新的速率信息与发射机相关参数信息写入SPDU中,随着邻近链路传输单元发送给接收机。发射机速率控制模块可以控制发射机的时钟模块、内插倍数、抽取倍数,控制整个发射机各模块的时钟速率,通过对内插倍数、抽取倍数的参数调整,控制发射机的采样率,是发射机满足CCSDS-211协议标准,支持1kbps、2kpbs、4kbps、8kbps~1024kbps、2048kbps范围中12档传输速率的切换。The transmitter adopts OQPSK modulation technology, adding a half-symbol period delay to the Q channel signal, so that the I channel and Q channel signals will not have polarity inversion at the same time, resulting in a 180° phase inversion, and the transmitted signal is first serial-parallel conversion to get The I channel and Q channel signals are then multiplied by the local transmitter NCO through modulation modules such as zero insertion, shaping filtering, and low-pass filtering to obtain the modulated OQPSK signal. The signal enters the deep space channel after digital up-conversion. . The transmitter has a transmitter rate control module, which can receive the rate feedback information sent by the receiver. The transmission rate of the transmitter is changed through the rate feedback information of the receiver, and at the same time, the new rate information of the transmitter and the relevant parameter information of the transmitter are written into the SPDU, and sent to the receiver along with the adjacent link transmission unit. The transmitter rate control module can control the clock module, interpolation multiple and decimation multiple of the transmitter, control the clock rate of each module of the entire transmitter, and control the sampling rate of the transmitter by adjusting the parameters of the interpolation multiple and decimation multiple. The transmitter complies with the CCSDS-211 protocol standard, and supports the switching of 12 transmission rates in the range of 1kbps, 2kpbs, 4kbps, 8kbps ~ 1024kbps, and 2048kbps.
接收机分为以下几个模块:数字下变频模块、增益检测模块、自动增益控制模块、载波同步模块、符号同步模块、帧同步模块、相位补偿与判决模块、串并转换模块、信噪比估计模块、接收机速率控制模块。The receiver is divided into the following modules: digital down-conversion module, gain detection module, automatic gain control module, carrier synchronization module, symbol synchronization module, frame synchronization module, phase compensation and decision module, serial-parallel conversion module, signal-to-noise ratio estimation module, receiver rate control module.
数字下变频模块将接收机接收到的信号转换为我们所需的低中频信号。The digital down-conversion module converts the signal received by the receiver into the low-IF signal we need.
增益检测模块对接收信号进行能量检测,当接收信号的能量高于预设的能量检测门限值时,判断接收信号属于有用用户信息,此时接收机开启;当接收信号的能量低于预设的能量检测门限值时,判断接收信号属于无效噪声,此时接收机关闭。检测门限值可以通过上层参数进行改变,使接收机在低功耗工作模式、正常工作模式间进行切换,满足不同情况下的接收机要求。The gain detection module performs energy detection on the received signal. When the energy of the received signal is higher than the preset energy detection threshold, it is judged that the received signal belongs to useful user information, and the receiver is turned on at this time; when the energy of the received signal is lower than the preset energy detection threshold When it reaches the energy detection threshold value, it is judged that the received signal is invalid noise, and the receiver is turned off at this time. The detection threshold value can be changed through the upper layer parameters, so that the receiver can switch between the low power consumption working mode and the normal working mode to meet the requirements of the receiver in different situations.
自动增益控制模块可以有效的控制接收机增益,当接收机接收信号由于信道衰落、宇宙噪音产生较大幅度的振荡时,自动增益控制模块会对增益系数进行自适应调整,防止信号饱和或丢失,使接收信号满足后级同步解调要求。The automatic gain control module can effectively control the gain of the receiver. When the received signal of the receiver oscillates with a large amplitude due to channel fading and cosmic noise, the automatic gain control module will adaptively adjust the gain coefficient to prevent signal saturation or loss. Make the received signal meet the requirements of post-stage synchronous demodulation.
本实施例的自动增益控制模块如图3所示,主要包括可控增益放大器、检测器模块、增益系数控制模块、比较器、误差处理模块。输入信号在经过A/D转换与可控增益放大器后进入检测器,检测器会对信号能量进行检测,输出信号一部分通过比较器与基准值进行比较,得到与基准值的误差,当误差较小时,可控增益放大器的增益系数保持不变,当误差超过阈值时,增益系数会根据误差处理模块反馈信息进行改变。同时检测器输出信号另一部分进入增益系数控制模块,对误差处理模块中的增益系数进行控制,自适应的改变误差处理模块的增益系数,增益系数控制模块根据检测值对误差处理模块中的增益系数进行调整时,其调整公式为Gain(n+1)=Gain(n)+aVe,其中,Gain(n+1)为调整后的增益系数,Gain(n)为当前增益系数,a为加权因子,Ve为与标准值误差。基于上述设计,面对输入数据较大幅度的震荡,可以使整个环路可以在较短的时间恢复稳定状态。误差处理模块接收增益控制模块与比较器器模块数据进行运算,得到新的可控增益放大器放大系数。As shown in FIG. 3 , the automatic gain control module of this embodiment mainly includes a controllable gain amplifier, a detector module, a gain coefficient control module, a comparator, and an error processing module. The input signal enters the detector after A/D conversion and controllable gain amplifier, the detector will detect the signal energy, part of the output signal is compared with the reference value through the comparator, and the error with the reference value is obtained, when the error is small , the gain coefficient of the controllable gain amplifier remains unchanged, and when the error exceeds the threshold, the gain coefficient will be changed according to the feedback information of the error processing module. At the same time, the other part of the output signal of the detector enters the gain coefficient control module, controls the gain coefficient in the error processing module, adaptively changes the gain coefficient of the error processing module, and the gain coefficient control module adjusts the gain coefficient in the error processing module according to the detected value. When adjusting, the adjustment formula is Gain(n+1)=Gain(n)+aV e , where Gain(n+1) is the adjusted gain coefficient, Gain(n) is the current gain coefficient, and a is the weighted factor, and Ve is the error from the standard value. Based on the above design, the entire loop can be restored to a stable state in a relatively short period of time in the face of relatively large oscillations of the input data. The error processing module receives the data of the gain control module and the comparator module and performs operations to obtain a new controllable gain amplifier amplification factor.
载波同步模块采用数字锁相环实现,通过对接收信号进行闭环检测,动态的调整接收机本地载波的频率,使其与发射机载波频率相等,使接收机后续模块可以进行相干解调。The carrier synchronization module is implemented by a digital phase-locked loop. Through closed-loop detection of the received signal, the frequency of the local carrier of the receiver is dynamically adjusted to make it equal to the carrier frequency of the transmitter, so that the subsequent modules of the receiver can perform coherent demodulation.
本实施例中,载波同步模块采用修正Costas环来实现,与普通Costas环和数字Costas环相比,修正Costas环具有较强的抗噪性能与较短的环路稳定时间。修正Costas环如图4所示,由本地NCO、匹配滤波器、数字鉴相器、环路滤波器组成,接收机接收到的I路、Q路信号经过匹配滤波器后进入数字鉴相器,所得到的鉴相器输出信号在经过环路滤波器后对接收机的本地NCO进行调整,直到接收机本地NCO与接收信号载波频率相一致后环路达到稳定。In this embodiment, the carrier synchronization module is implemented by the modified Costas loop. Compared with the ordinary Costas loop and the digital Costas loop, the modified Costas loop has stronger anti-noise performance and shorter loop stabilization time. The modified Costas loop is shown in Figure 4. It consists of a local NCO, a matched filter, a digital phase detector, and a loop filter. The I and Q signals received by the receiver enter the digital phase detector after passing through the matched filter. The obtained output signal of the phase detector adjusts the local NCO of the receiver after passing through the loop filter, until the local NCO of the receiver is consistent with the carrier frequency of the received signal, the loop becomes stable.
本发明为了获取最佳采样点,采用迟早环算法进行符号同步设计,通过调整采样率便可实现高精度的符号同步。迟早环符号同步结构如图5所示,主要包括早门积分电路、迟门积分电路、数据误差鉴别器、环路滤波器、锁定判决器与时钟发生器。对I路、Q路信号进行归一化处理,处理后所得方波信号进入早门积分电路与迟门积分电路,在经过数据误差鉴别器进行判决,当存在时钟误差时,该算法会迅速累积误差,数据误差鉴别器会给出误差数据,在经过环路滤波器后对时钟发生器进行调整,改变时钟频率,直到得到最佳采样时刻,同时,锁定判决器会给出锁定指示,清楚的反应符号同步模块的工作状态。In order to obtain the best sampling point, the present invention adopts the sooner or later loop algorithm to design the symbol synchronization, and can realize the high-precision symbol synchronization by adjusting the sampling rate. The symbol synchronization structure of the sooner or later loop is shown in Figure 5, which mainly includes an early gate integrator circuit, a late gate integrator circuit, a data error discriminator, a loop filter, a lock decision device and a clock generator. The I channel and Q channel signals are normalized, and the square wave signal obtained after processing enters the early gate integrator circuit and the late gate integrator circuit, and is judged by the data error discriminator. When there is a clock error, the algorithm will quickly accumulate Error, the data error discriminator will give error data, adjust the clock generator after passing through the loop filter, change the clock frequency until the best sampling time is obtained, at the same time, the lock judger will give a lock indication, clear Indicates the working status of the symbol synchronization module.
CCSDS-211协议采用附加同步标志位(ASM)作为传输帧的帧头,本发明采用帧同步模块准确定位数据信息中的ASM位置,保障后续信号处理的可靠性。The CCSDS-211 protocol adopts the additional synchronization flag (ASM) as the frame header of the transmission frame, and the present invention adopts the frame synchronization module to accurately locate the ASM position in the data information to ensure the reliability of subsequent signal processing.
本发明具有相位补偿与判决模块,有效地消除OQPSK信号在传输过程中发生的极性翻转所带来90°的相位误差,通过对相位偏差的估计进行补偿,之后进行判决得到用户比特信息,有效地降低了系统误码率,保障了系统的有效性与可靠性。The present invention has a phase compensation and judgment module, which effectively eliminates the 90° phase error caused by the polarity inversion of the OQPSK signal during the transmission process, compensates for the phase deviation estimation, and then judges to obtain user bit information, effectively Therefore, the bit error rate of the system is greatly reduced, and the effectiveness and reliability of the system are guaranteed.
相位补偿与判决后的信号经过串并转换后输出用户信息。The signal after phase compensation and judgment is serial-parallel converted and then output user information.
本发明包括信噪比估计模块,对所接收到的信号进行信噪比估计,判断信道当前通信质量。本发明采用DF-3估计与SNV估计相结合的信噪比估计算法,利用在0~10dB情况下DF-3估计性能优越与10dB以上时SNV估计性能优越,将DF-3估计算法与SNV估计算法相结合,得到一种硬件复杂度较低的,信噪比估计误差较小的信噪比联合估计算法。如图6所示,该算法首先将上一时刻信噪比估计值作为信噪比反馈信息输入信噪比估计算法选择模块,通过对比信噪比反馈信息与模块内所设定的门限值选择后级相应信噪比估计算法,当信噪比发生变化超过门限值时,信噪比估计算法会在下一时刻进行切换,可以使输入信号在不同信噪比情况下都能选择误差较小的信噪比估计算法进行估计。例如:以10dB为门限,高于10dB时选用SNV估计,0~10dB选用DF-3估计,前一时刻信噪比决定下一时刻信噪比估计方法,当前信噪比由所选信噪比估计算法计算得出。The present invention includes a signal-to-noise ratio estimation module, which estimates the signal-to-noise ratio of the received signal and judges the current communication quality of the channel. The present invention adopts the signal-to-noise ratio estimation algorithm combining DF-3 estimation and SNV estimation, utilizes the superior performance of DF-3 estimation under the condition of 0-10 dB and the superior SNV estimation performance under the condition of 10 dB or more, and combines the DF-3 estimation algorithm with SNV estimation Combining the algorithms, a SNR joint estimation algorithm with lower hardware complexity and smaller SNR estimation error is obtained. As shown in Figure 6, the algorithm first takes the estimated value of the signal-to-noise ratio at the previous moment as the feedback information of the signal-to-noise ratio into the signal-to-noise ratio estimation algorithm selection module, and compares the feedback information of the signal-to-noise ratio with the threshold value set in the module. Select the corresponding signal-to-noise ratio estimation algorithm in the later stage. When the signal-to-noise ratio changes beyond the threshold value, the signal-to-noise ratio estimation algorithm will be switched at the next moment, so that the input signal can choose the error comparison under different signal-to-noise ratio conditions. A small signal-to-noise ratio estimation algorithm is used for estimation. For example: take 10dB as the threshold, use SNV estimation when it is higher than 10dB, DF-3 estimation is used for 0~10dB, the SNR at the previous moment determines the SNR estimation method at the next moment, and the current SNR is determined by the selected SNR Calculated by the estimation algorithm.
本发明设计发射机速率控制模块和接收机速率控制模块,通过上位机的误码率要求与信噪比估计模块的输出信噪比,自适应的调整码元速率。通过上位机发来的误码率要求计算出所需信噪比大小,再与信噪比估计模块的输出信噪比比较,利用OQPSK信号降低一半符号速率信噪比提升3dB,升高一倍符号速率信噪比降低3dB的特点,对信号速率进行逐级调整,直至信噪比达到所需信噪比要求。本发明对误码率要求10-7,初始信噪比28dB,初始数据速率64kbps进行了仿真,验证了该自适应变速率系统可以通过上位机误码率要求与当前信道信噪比来自适应的调整数据速率,使收发机在满足误码率要求的前提下尽可能的提升吞吐量,保障了通信系统的有效性跟可靠性。The invention designs a transmitter rate control module and a receiver rate control module, and adjusts the symbol rate adaptively according to the bit error rate requirement of the upper computer and the output signal-to-noise ratio of the signal-to-noise ratio estimation module. Calculate the required signal-to-noise ratio through the bit error rate request sent by the host computer, and then compare it with the output signal-to-noise ratio of the signal-to-noise ratio estimation module, and use the OQPSK signal to reduce the symbol rate by half and increase the signal-to-noise ratio by 3dB and double. The signal-to-noise ratio of the symbol rate is reduced by 3dB, and the signal rate is adjusted step by step until the signal-to-noise ratio reaches the required signal-to-noise ratio requirement. The present invention simulates the bit error rate requirement of 10 -7 , the initial signal-to-noise ratio of 28dB, and the initial data rate of 64kbps, and verifies that the self-adaptive variable rate system can be adapted by the bit error rate requirement of the upper computer and the signal-to-noise ratio of the current channel. The data rate is adjusted so that the transceiver can improve the throughput as much as possible on the premise of meeting the bit error rate requirements, which ensures the effectiveness and reliability of the communication system.
下面通过具体实验数据进一步验证本发明的技术效果。The technical effect of the present invention is further verified below through specific experimental data.
OQPSK在高斯信道下的误码率曲线特性如图7所示,因此,在本实验中,根据误码率要求10-7计算得出满足当前误码率要求的信噪比为14.5dB,增加1dB容错,将信噪比门限值设为15.5dB。The bit error rate curve characteristics of OQPSK under the Gaussian channel are shown in Figure 7. Therefore, in this experiment, according to the bit error rate requirement of 10 -7 , the SNR that meets the current bit error rate requirement is calculated to be 14.5dB. 1dB fault tolerance, set the signal-to-noise ratio threshold to 15.5dB.
图8为误码率要求10-7,初始信噪比28dB,初始数据速率512kbps自适应变速率仿真图。当前信噪比高于门限值3dB时,提高一倍符号速率,提高系统吞吐量;当前信噪比低于门限值时,降低一半符号速率,以满足系统信噪比要求;当前信噪比高于门限值3dB以内时,符号速率保持不变,系统达到最优性能。由仿真图可以看出,初始信噪比较高,当前信道环境良好,通过逐级提高符号速率,将初始速率64kbps提高到1024kbps,极大的提高了系统吞吐量,同时,信噪比仍满足系统误码率要求,所设计系统具有优越的性能。Fig. 8 is a simulation diagram of a bit error rate requirement of 10 -7 , an initial signal-to-noise ratio of 28dB, and an initial data rate of 512kbps adaptive variable rate. When the current SNR is higher than the threshold by 3dB, the symbol rate is doubled to improve the system throughput; when the current SNR is lower than the threshold, the symbol rate is reduced by half to meet the system SNR requirements; the current SNR When the ratio is higher than the threshold value within 3dB, the symbol rate remains unchanged, and the system achieves the optimal performance. It can be seen from the simulation diagram that the initial signal-to-noise ratio is high, and the current channel environment is good. By increasing the symbol rate step by step, the initial rate of 64kbps is increased to 1024kbps, which greatly improves the system throughput. At the same time, the signal-to-noise ratio is still satisfactory. System bit error rate requirements, the designed system has superior performance.
以上所述仅是本发明的优选实施方式,应当指出:对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only the preferred embodiment of the present invention, it should be pointed out that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can also be made, and these improvements and modifications are also It should be regarded as the protection scope of the present invention.
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114185825A (en) * | 2021-10-25 | 2022-03-15 | 西安空间无线电技术研究所 | Architecture system based on multi-service working mode |
RU2797257C1 (en) * | 2022-11-01 | 2023-06-01 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Radio pulse receiver |
CN117768011A (en) * | 2024-02-22 | 2024-03-26 | 长光卫星技术股份有限公司 | FPGA-based adaptive transmission system, method, equipment and medium |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1703859A (en) * | 2002-02-28 | 2005-11-30 | 英特尔公司 | Data transmission rate control using an estimation of the SNR of the communication channel |
CN1802828A (en) * | 2003-06-11 | 2006-07-12 | 皇家飞利浦电子股份有限公司 | Receiver for a multi-carrier communication system |
CN101369898A (en) * | 2008-09-12 | 2009-02-18 | 中国电子科技集团公司第五十四研究所 | Meteor trail self-adapting variable-velocity burst modem |
CN102075472A (en) * | 2011-02-16 | 2011-05-25 | 四川九洲电器集团有限责任公司 | Method for spreading intermediate frequency of OQPSK and despreading and demodulating spread intermediate frequency |
CN104683071A (en) * | 2015-03-17 | 2015-06-03 | 中国电子科技集团公司第五十四研究所 | Self-adaptive variable rate device for burst asymmetric channels |
CN107204826A (en) * | 2017-03-30 | 2017-09-26 | 南京航空航天大学 | Towards the ADAPTIVE MIXED repeating method and device of deep space communication |
-
2019
- 2019-10-17 CN CN201910991741.3A patent/CN110943752A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1703859A (en) * | 2002-02-28 | 2005-11-30 | 英特尔公司 | Data transmission rate control using an estimation of the SNR of the communication channel |
CN1802828A (en) * | 2003-06-11 | 2006-07-12 | 皇家飞利浦电子股份有限公司 | Receiver for a multi-carrier communication system |
CN101369898A (en) * | 2008-09-12 | 2009-02-18 | 中国电子科技集团公司第五十四研究所 | Meteor trail self-adapting variable-velocity burst modem |
CN102075472A (en) * | 2011-02-16 | 2011-05-25 | 四川九洲电器集团有限责任公司 | Method for spreading intermediate frequency of OQPSK and despreading and demodulating spread intermediate frequency |
CN104683071A (en) * | 2015-03-17 | 2015-06-03 | 中国电子科技集团公司第五十四研究所 | Self-adaptive variable rate device for burst asymmetric channels |
CN107204826A (en) * | 2017-03-30 | 2017-09-26 | 南京航空航天大学 | Towards the ADAPTIVE MIXED repeating method and device of deep space communication |
Non-Patent Citations (3)
Title |
---|
居行波: ""基于FPGA的邻近空间自适应传输关键技术研究与实现"", 《中国优秀硕士学位论文全文数据库(信息科技辑)》 * |
李松等: ""基于CCSDS的自适应传输系统设计及实现"", 《航空兵器》 * |
谷雨: ""深空通信调制解调系统的设计与实现"", 《中国优秀硕士学位论文全文数据库(信息科技辑)》 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114185825A (en) * | 2021-10-25 | 2022-03-15 | 西安空间无线电技术研究所 | Architecture system based on multi-service working mode |
CN114185825B (en) * | 2021-10-25 | 2024-05-03 | 西安空间无线电技术研究所 | Architecture system type system based on multi-service working mode |
RU2797257C1 (en) * | 2022-11-01 | 2023-06-01 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Radio pulse receiver |
CN117768011A (en) * | 2024-02-22 | 2024-03-26 | 长光卫星技术股份有限公司 | FPGA-based adaptive transmission system, method, equipment and medium |
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