Journals Articles Conferences News About CLP
Submit a paper Email Alert
Search
Search
Articles
Journals
News
Advanced Search
Top Searches
2D MaterialsTransformation opticsQuantum PhotonicsSmall lasersSemiconductor UV PhotonicsSupersymmetric microring laser arrays

Laser & Optoelectronics Progress, Volume. 59, Issue 19, 1912003(2022)

Research and Application of Lunar Laser Ranging Observation Model

Kai Huang1,3, Shangbiao Sun2, Yongzhang Yang1, Rufeng Tang1, Zhulian Li1, and Yuqiang Li1、*
Author Affiliations
  • 1Yunnan Observatories, Chinese Academy of Sciences, Kunming 650216, Yunnan, China
  • 2State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, Hubei, China
  • 3School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China
    • show less
    AbstractGet PDF(in Chinese)
    Figures&Tables (11)
    Equations (10)
    References (14)
    Cited By (2)
    Tools
    Paper Information
    Topics
    Figures & Tables(11)
    Basic principle of the LLR

    Fig. 1. Basic principle of the LLR

    Download full size
    Time difference calculated by SOFA and INPOP19a methods

    Fig. 2. Time difference calculated by SOFA and INPOP19a methods

    Download full size
    Variation of the position of the corner reflector caused by lunar solid tide

    Fig. 3. Variation of the position of the corner reflector caused by lunar solid tide

    Download full size
    Two-way residuals of LLR data

    Fig. 4. Two-way residuals of LLR data

    Download full size
    Two-way residuals of LLR data from Yunnan Observatory

    Fig. 5. Two-way residuals of LLR data from Yunnan Observatory

    Download full size
    Standard point data processing results under different inputs. (a) INPOP19a; (b) EPM2017; (c) DE430; (d) standard point data difference between INPOP19a and EPM2017; (e) standard point data difference between INPOP19a and DE430; (f) standard point data difference between DE430 and EPM2017

    Fig. 6. Standard point data processing results under different inputs. (a) INPOP19a; (b) EPM2017; (c) DE430; (d) standard point data difference between INPOP19a and EPM2017; (e) standard point data difference between INPOP19a and DE430; (f) standard point data difference between DE430 and EPM2017

    Download full size
    Difference between the predicted position at launch time and the CPF file

    Fig. 7. Difference between the predicted position at launch time and the CPF file

    Download full size
    Difference between the forecast position at the time of reception and the CPF file

    Fig. 8. Difference between the forecast position at the time of reception and the CPF file

    Download full size

    • Table 1. Reference systems used by the generative model

      View table

      Table 1. Reference systems used by the generative model

      ComponentReference
      Lunar orbit around the earthINPOP19a
      Lunar librationINPOP19a
      Earth rotation and orientationIERS Conv.（2010）
      Relativistic propagation delayIERS Conv.（2010）
      Lorentz transform between TDB and TTIERS Conv.（2010）
      Solid earth tidesIERS Conv.（2010）
      Solid moon tidesLove number estimated with INPOP19a
      Atmospheric delayIERS Conv.（2010）

    • Table 2. Three-dimensional coordinates and average moving speed of ground station under ITRF

      View table

      Table 2. Three-dimensional coordinates and average moving speed of ground station under ITRF

      Earth stationX /mY /mZ /mX˙ /（mm·a-1）Y˙/（mm·a-1）Z˙ /（mm·a-1）
      Apollo-1463998.9085-5166632.76353435012.8835-0.01410.0003-0.0022
      Grasse4581692.1675556196.07304389355.1088-0.01510.01910.0118
      Haleakala-5466003.7191-2404425.93692242197.9030-0.01220.06220.0310
      Matera4641978.81001393067.53104133249.4800-0.01800.01920.0140
      McDonald-1330781.5567-5328756.37833235697.9118-0.02770.02770.0139
      MLRS 1-1330120.9826-5328532.36443236146.0080-0.01240.0009-0.0053
      MLRS 2-1330021.4931-5328403.34013236481.6472-0.01290.0015-0.0036
      Wettzell4075576.7587931785.50774801583.6067-0.01390.01700.0124

    • Table 3. Three-dimensional coordinates of reflector under PA

      View table

      Table 3. Three-dimensional coordinates of reflector under PA

      Lunar reflectorX /mY /mZ /m
      Apollo 111591966.6111690699.545221003.7497
      Lunokhod 11114292.2641-781298.38441076058.6360
      Apollo 141652689.5835-520997.5017-109730.5271
      Apollo 151554678.304798095.6097765005.2064
      Lunokhod 21339363.3642801872.0049756358.6487
    Tools

    Get Citation

    Copy Citation Text

    Kai Huang, Shangbiao Sun, Yongzhang Yang, Rufeng Tang, Zhulian Li, Yuqiang Li. Research and Application of Lunar Laser Ranging Observation Model[J]. Laser & Optoelectronics Progress, 2022, 59(19): 1912003

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Set citation alerts for article
    Save article for my favorites
    Paper Information

    Category: Instrumentation, Measurement and Metrology

    Received: Sep. 13, 2021

    Accepted: Oct. 19, 2021

    Published Online: Sep. 23, 2022

    The Author Email: Li Yuqiang (lyq@ynao.ac.cn)

    DOI:10.3788/LOP202259.1912003

    Topics

    laser devices and laser physics
    Lasers and Laser Optics
    Laser physics
    laser manufacturing
    Instrumentation, Measurement and Metrology