The Uplink VLBI Receiving System for Deep Space Exploration in the Spacecraft

被引:0
|
作者
Xue, Linshan [1 ]
Li, Xue [2 ]
Wu, Weiren [3 ,4 ]
Wang, Lu [1 ]
Zhang, Jianjun [1 ]
机构
[1] China Acad Space Technol CAST, Beijing 100081, Peoples R China
[2] Chongqing Univ, Ctr Commun & Tracking Telemetry Command, Chongqing 400044, Peoples R China
[3] Univ Elect Sci & Technol China, Sch Mech & Elect Engn, Chengdu 611731, Peoples R China
[4] Lunar Explorat & Space Engn Ctr, Beijing 100190, Peoples R China
关键词
Carrier phase measurement; deep space navigation; phase ambiguity resolution; telemetry tracking and command (TT&C); very long baseline interferometry (VLBI); SAME-BEAM VLBI; INTERFEROMETRY; SIMULATION;
D O I
10.1109/TIM.2024.3472784
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In deep space telemetry tracking and command (TT&C) missions, the low signal-to-noise ratio (SNR) of the receiving signal restricts the improvement of measurement performance. In the article, we adopt the uplink signal which transmitted by the ground station to achieve very long baseline interferometry (VLBI) in the spacecraft. Notably, this methodology guarantees an SNR enhancement of at least 30 dB compared to the downlink signal, marking a significant improvement. Considering the restrict of spacecraft calculate resources, we adopt multiple baselines to simplify the VLBI method in spacecraft receiver and obtain the high accuracy angle measurement results. The simulation and analysis show that the algorithm achieves a measurement accuracy of 0.77 nrad on the baseline length of 74 km, while the accuracy of traditional delta differential one-way ranging (Delta DOR) observations is 1 nrad with an 8400 km baseline length. In addition, we design a hardware platform for algorithm verification. This platform, under real-world conditions, exhibits an angle measurement error of less than 5 mrad even with a baseline length as short as 0.74 m.
引用
收藏
页数:11
相关论文
共 50 条
  • [41] Design and implementation of a planetary data system for Chinese deep space exploration
    Li C.
    Yao P.
    Liu X.
    Chen B.
    Zou H.
    Wang B.
    Zhang J.
    Li B.
    Ling Z.
    Chen S.
    Li, Bo (libralibo@sdu.edu.cn), 1600, (25): : 599 - 613
  • [42] A Spacecraft Electric Propulsion System Using Hybrid Excitation Generator for Deep Space Missions
    Gholamian, Mahzad
    Beik, Omid
    Talebzadeh, Sarah
    Sarfi, Ghazaleh
    2024 IEEE AEROSPACE CONFERENCE, 2024,
  • [43] Resilience evaluation of the environmental control and life support system of a spacecraft for deep space travel
    Matelli, Jose Alexandre
    Goebel, Kai
    ACTA ASTRONAUTICA, 2018, 152 : 360 - 369
  • [44] Geometric effects on deep space orbit determination via Space-VLBI observations
    Asai, Y
    Nishimura, T
    Kamijo, F
    Hoshino, U
    SICE 2002: PROCEEDINGS OF THE 41ST SICE ANNUAL CONFERENCE, VOLS 1-5, 2002, : 175 - 180
  • [45] Efficient design techniques for cislunar-space VLBI spacecraft formation in GTOC8
    He, Shengmao
    Zhu, Zhengfan
    ASTRODYNAMICS, 2021, 5 (01) : 61 - 76
  • [46] Effects of space environments on space laser system for spacecraft
    Shen, Zicai
    Wang, Yanzhi
    Zhao, Chunqing
    Ding, Yigang
    HIGH-POWER LASERS AND APPLICATIONS XI, 2020, 11544
  • [47] Investigation on the development of deep space exploration
    WU WeiRen LIU WangWang QIAO Dong JIE DeGang School of Aerospace Engineering Beijing Institute of Technology Beijing China Center of Lunar Exploration and Aerospace Engineering Beijing China
    Science China(Technological Sciences), 2012, 55 (04) : 1086 - 1091
  • [48] Vision and Voyages for Deep Space Exploration
    ZOU Yongliao
    WANG Qin
    空间科学学报, 2016, (05) : 606 - 609
  • [49] Investigation on the development of deep space exploration
    WeiRen Wu
    WangWang Liu
    Dong Qiao
    DeGang Jie
    Science China Technological Sciences, 2012, 55 : 1086 - 1091
  • [50] Deep space environments for human exploration
    Wilson, JW
    Clowdsley, MS
    Cucinotta, FA
    Tripathi, RK
    Nealy, JE
    De Angelis, G
    SPACE LIFE SCIENCES: RADIATION RISK ASSESSMENT AND RADIATION MEASUREMENT IN LOW EARTH ORBIT, 2004, 34 (06): : 1281 - 1287