Design and Simulation of Low-Orbit Satellite Broadcast Signal Receiving and Processing Terminal

被引:0
|
作者
Shen, Haoran [1 ]
Li, Jian [1 ]
Wang, Ziwei [1 ]
机构
[1] Radar Technol Res Inst, Beijing Inst Technol, Sch Informat & Elect, Minist Educ, Beijing 100081, Peoples R China
关键词
time-frequency domain interference suppression; beam synthesis; acquisition tracking; bit synchronization loop; simulation design;
D O I
10.3390/electronics13163270
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
As an important space-based intelligence acquisition and combat command receiving component, the low-orbit satellite broadcast signal receiving terminal is an important guarantee for realizing the full-dimensional joint operations of our military's multi-services. This design is based on the SoC platform. Compared to the traditional low-orbit reconnaissance satellite reception and processing terminal business process, a narrowband anti-interference module is added and the interference-to-signal ratio reaches 57 dB and 47 dB when resisting interference from a single frequency band and three frequency bands, respectively. Digital beamforming is used for signal processing and beamforming gain of the whole machine reaches 14-15 dBic; compared to traditional capture and tracking modules, this terminal uses a time domain parallel frequency domain FFT fast acquisition method and a bit synchronization loop is added to the tracking loop to aiming at the problem that the frequency signal acquisition speed is not fast enough and addressing the issue that information symbol rate is not an integer multiple of the pseudo-code, thus complete bit synchronization within 60 ms, with a bit error rate of 0; the coding gain can reach 7 dB. Combined with the solution of decoding and positioning solution algorithms, this scheme used the JFM7K325T chip to complete the design simulation of the complete receiving and processing terminal.
引用
收藏
页数:23
相关论文
共 50 条
  • [31] POWER-SYSTEM SIMULATION FOR LOW-ORBIT SPACECRAFT - THE EBLOS COMPUTER-PROGRAM
    CAPEL, A
    FERRANTE, J
    CORNET, J
    LEBLANC, P
    ESA JOURNAL-EUROPEAN SPACE AGENCY, 1982, 6 (03): : 319 - 337
  • [32] Design and validation of broadcast ephemeris for low Earth orbit satellites
    Xie, Xin
    Geng, Tao
    Zhao, Qile
    Liu, Xianglin
    Zhang, Qiang
    Liu, Jingnan
    GPS SOLUTIONS, 2018, 22 (02)
  • [33] Design and validation of broadcast ephemeris for low Earth orbit satellites
    Xin Xie
    Tao Geng
    Qile Zhao
    Xianglin Liu
    Qiang Zhang
    Jingnan Liu
    GPS Solutions, 2018, 22
  • [34] Research on Detection Capability of Low-Orbit Infrared Satellite to HTV-2-Like Hypersonic Vehicle
    Chen H.
    Zhang A.
    Liu X.
    Li J.
    Li S.
    Guangxue Xuebao/Acta Optica Sinica, 2021, 41 (21):
  • [35] Research on Routing Equalization Algorithm of Inter-Satellite Partition for Low-Orbit Micro-Satellites
    Cheng, Hengfei
    Xu, Zhaobin
    Guo, Xiaoxu
    Yang, Jia
    Xu, Kedi
    Liu, Shuqin
    Jin, Zhonghe
    Jin, Xiaojun
    FUTURE INTERNET, 2022, 14 (07):
  • [36] Attitude planning and control method of low-orbit optical satellite along-track stereoscopic imaging
    Li F.
    Wan Q.
    Liu M.
    Zhong X.
    Qu Y.
    Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2022, 30 (14): : 1682 - 1693
  • [37] Load Balancing Routing Algorithm of Low-Orbit Communication Satellite Network Traffic Based on Machine Learning
    Liu, Tie
    Sun, Chenhua
    Zhang, Yasheng
    WIRELESS COMMUNICATIONS & MOBILE COMPUTING, 2021, 2021
  • [38] Low-orbit satellite momentum unloading using gravity gradient and solar-panel aerodynamic torques
    Guo, Jian
    Yang, Baoqing
    Yao, Yu
    Zhao, Hui
    Wang, Xingdan
    Liu, Kai
    1600, ICIC Express Letters Office, Tokai University, Kumamoto Campus, 9-1-1, Toroku, Kumamoto, 862-8652, Japan (07): : 2121 - 2127
  • [39] ORBIT DESIGN AND SIMULATION FOR KUFASAT NANO-SATELLITE
    Mahdi, Mohammed Chessab
    ARTIFICIAL SATELLITES-JOURNAL OF PLANETARY GEODESY, 2015, 50 (04): : 157 - 168
  • [40] Satellite orbit modeling and simulation for mission analysis and design
    Chouraqui, S
    Underwood, CI
    MESM '2004: 6th Middle East Simulation Multiconference, 2004, : 76 - 80