High Performance Real-time Odd-even Channels Combination Algorithm for Transmission Baseband Data Using Dual-polarized Technology
-
摘要: 数传基带奇偶合路实时处理,是极化复用方式下卫星过境弧段即时判读星载设备状态及获取空间科学探测成果的前提和基础。面向空间科学卫星高速数传实时处理需求,针对传统合路处理方法受限于内存拷贝与排序操作导致处理性能较低的问题,提出一种使用环形队列对数据进行内存管理并基于各虚拟信道奇偶单路传输帧计数自然有序特征进行合路处理的新方法,有效规避频繁的内存移动与复杂耗时的排序操作,显著提升奇偶合路实时处理性能。空间科学卫星任务的工程实践结果表明,所提方法的实时合路性能满足ASO-S卫星1 Gbit·s–1和CASEarth卫星1.6 Gbit·s–1的高速数传实时处理需求。Abstract: Odd-even frames real-time combination for transmission baseband data which used dual-polarized technology is the prerequisite and basis for timely monitoring of satellite equipment status when the satellite is in transit arc and early access to scientific exploration data by satellite ground application system. A high performance real-time odd-even channels combination algorithm for transmission baseband data which uses dual-polarized technology is proposed to meet the need of scientific satellite real-time high-speed data processing. This method makes full use of the naturally ordered frame counting feature of each virtual channel and applies the circular memory management design of circular queue. Therefore, this method effectively avoids the time-consuming sort and frequent memory moving operations compared to traditional algorithms. The space science satellites’ engineering practice shows that the speed of combination meets ASO-S’s 1 Gbit s–1 and CASEarth’s 1.6 Gbit s–1 real-time processing requirements.
-
Key words:
- Dual-polarized technology /
- Real-time odd-even channels combination /
- Circular queue /
- ASO-S /
- CASEarth
-
表 1 测试数据统计
Table 1. Statistics of test data
通道 文件大小
/GByte同步码
计数填充信道帧
第一帧计数实时工程
参数帧计数回放工程
参数帧计数载荷科学
数据帧计数奇路 29 29 959 953 813 1502 71 225 10 983 970 偶路 29 29 925 282 69 682 1502 71 225 10 983 970 -
[1] 王中果, 汪大宝, 胡月, 等. 低轨遥感卫星Ka频段自适应编码调制应用效能分析[J]. 航天器工程, 2021, 30(4): 69-76 doi: 10.3969/j.issn.1673-8748.2021.04.010WANG Zhongguo, WANG Dabao, HU Yue, et al. Analysis on application efficiency of adaptive coding and modulation for LEO remote sensing satellite at Ka-band[J]. Spacecraft Engineering, 2021, 30(4): 69-76 doi: 10.3969/j.issn.1673-8748.2021.04.010 [2] GENEVA, ITU. ITU Radio communication (ITU-R). Radio regulations articles edition of 2020[S]. 2020 [3] 郭道省, 张晓凯, 张邦宁, 等. 极化特性在卫星通信系统中的应用研究[J]. 无线电通信技术, 2018, 44(3): 211-216 doi: 10.3969/j.issn.1003-3114.2018.03.01GUO Daoxing, ZHANG Xiaokai, ZHANG Bangning, et al. Study of polarization feature in satellite communication[J]. Radio Communications Technology, 2018, 44(3): 211-216 doi: 10.3969/j.issn.1003-3114.2018.03.01 [4] 徐崇彦, 张言锋, 闫东磊. 极化复用在遥感卫星接收系统中的工程化应用[J]. 无线电工程, 2017, 47(3): 75-78 doi: 10.3969/j.issn.1003-3106.2017.03.19XU Chongyan, ZHANG Yanfeng, YAN Donglei. The engineering application of dual-polarized technology in remote sensing satellite receiving system[J]. Radio Engineering, 2017, 47(3): 75-78 doi: 10.3969/j.issn.1003-3106.2017.03.19 [5] 赵宁. 极化复用技术在遥感卫星数据传输中的应用[J]. 航天器工程, 2010, 19(4): 55-62 doi: 10.3969/j.issn.1673-8748.2010.04.009ZHAO Ning. Application of dual-polarized technology in remote sensing satellite data transmission[J]. Spacecraft Engineering, 2010, 19(4): 55-62 doi: 10.3969/j.issn.1673-8748.2010.04.009 [6] GAN W Q, ZHU C, DENG Y Y, et al. Advanced space-based solar observatory (ASO-S): an overview[J]. Research in Astronomy and Astrophysics, 2019, 19(11): 156 doi: 10.1088/1674-4527/19/11/156 [7] GUO H D, CHEN H Y, CHEN L F, et al. Progress on CASEarth satellite development[J]. Chinese Journal of Space Science, 2020, 40(5): 707-717 [8] CCSDS. CCSDS 732.0-P-3.1 AOS space data link protocol[S]. Washington: National Aeronautics and Space Administration, 2021 [9] 马苗, 朱岩. 基于CCSDS标准的卫星数据处理软件设计[J]. 电子设计工程, 2015, 23(1): 16-20 doi: 10.3969/j.issn.1674-6236.2015.01.006MA Miao, ZHU Yan. Design of satellite data processing software based on CCSDS[J]. Electronic Design Engineering, 2015, 23(1): 16-20 doi: 10.3969/j.issn.1674-6236.2015.01.006 [10] 郑娟, 祝彬, 陆静, 等. AOS(高级在轨系统)协议跟踪研究[J]. 航天标准化, 2016(4): 33-38,45 doi: 10.3969/j.issn.1009-234X.2016.04.009ZHENG Juan, ZHU Bin, LU Jing, et al. AOS protocol tracking research[J]. Aerospace Standardization, 2016(4): 33-38,45 doi: 10.3969/j.issn.1009-234X.2016.04.009 -