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Single Station GPS Ionospheric Corrections Joe Malins 12/9/2016 - PowerPoint PPT Presentation

Single Station GPS Ionospheric Corrections Joe Malins 12/9/2016 1 1 Statement of Problem Want Faraday rotation to measure magnetic field of sun and CMEs Currently: IONEX Files: use global models involving hundreds of GPS


  1. Single Station GPS Ionospheric Corrections Joe Malins 12/9/2016 1 1

  2. Statement of Problem • Want Faraday rotation to measure magnetic field of sun and CMEs • Currently: IONEX Files: • use global models involving hundreds of GPS stations • Problem: not many GPS receivers located near LWA Stovall, Kevin (UNM) • Problem: Global models JPL Global Ionospheric TEC Map update approximately every hour. • Time of Appreciable Change ~10 min 2 12/9/2016 2

  3. Equipment LWA Dual Frequency GPS Antenna • NovAtel 4004B Dual Frequency GPS • Borrowed from Air Force Research Lab Scintillation Network Decision Aid (SCINDA) program • Self-biasing, 10s resolution, Plasmasphere correction 12/9/2016 3 3

  4. RM measurement • Using Polarized Pulsars • Three contributions to rotation measure: • Material surrounding pulsar • Interstellar/Interplanetary Medium • Ionosphere and near earth plasma • Assume near constant ISM and material surrounding pulsar • or at least changing on long time scales See Veronica Dike (UNM) Poster • At large sun angles Short time scale change only due to ionosphere • Find rotation measure, measure ionospheric contribution, fit RM curve to ionosphere 4 12/9/2016 4

  5. Ionosphere Measurement • Dual Frequency: 1575.42 MHz and 1227.60 MHz Different frequencies are GPS delayed different amounts • Ionosphere is plasma • Plasmas causes group velocity delay, phase velocity increase in EM waves • Delays are strongly frequency Ionosphere dependent • Integrated electron density: Lower ν is delayed more Total Electron Content (TEC) • Measured in n e /m 2 or TEC units (TECU) 1 TECU = 10 16 n e /m 2 • No profile information Receiver 5 12/9/2016 5

  6. Better Corrections Interpolated Observation at LWA1 at 2016/10/14 12:00:00 UTC • Each satellite provides accurate data to a single point on the sky • Between 7-14 satellites at any given time • For points between satellites, use linear weighted average of satellites 𝑈𝐹𝐷 = ∑ 𝜍 𝑈𝐹𝐷 1 𝑒 𝑚 1 𝜍 = ∑ 1 𝑒 𝑚 6 12/9/2016 6

  7. CODE Model JPL Model 1.4 2.0 1.0 0.6 𝜓 2 = 3.5999 𝑛 2 𝜓 2 = 0.6725 𝑠𝑏𝑒 RM: GPS Observation 2.0 Pulsar: B0950+08 3x 2Hour Observations (Black Dashed Lines) Date: 2016/09/23 1.0 𝜓 2 = 0.3061 12/9/2016 7

  8. CODE Model JPL Model 1.6 2.5 0.8 1.0 𝜓 2 = 3.6780 𝜓 2 = 1.4576 𝑛 2 𝑠𝑏𝑒 RM: GPS Observation 2.0 Pulsar: B0950+08 3x 2Hour Observations (Black Dashed Lines) Date: 2016/10/05 1.0 𝜓 2 = 0.2520 12/9/2016 8

  9. JPL Model CODE Model 3.0 3.5 1.5 1.5 𝑛 2 𝑠𝑏𝑒 𝜓 2 = 25.2052 𝜓 2 = 1.6509 RM: GPS Observation 4.0 Pulsar: B0950+08 3x 2Hour Observations (Black Dashed Lines) Date: 2016/10/14 2.0 𝜓 2 = 0.7628 12/9/2016 9

  10. Height Dependence • Current model : Thin Shell Model • Attempt electrons distributed along profile • 1 st Try: • 191 points along C. Sotomayor-Beltran et al.: Ionospheric Faraday rotation International Reference Ionosphere (IRI) • 2 nd Try: • AFRL Ionosonde data from AFRL at Kirtland 10 12/9/2016 10

  11. 2016/09/23 GPS with height correction GPS without height correction Height Corrected Not Height Corrected 𝑛 2 𝑠𝑏𝑒 RM: Height Corrected: 𝜓 2 = 0.5631 Not Height Corrected: 𝜓 2 = 0.3061 12/9/2016 11 11

  12. 2016/10/05 Height Corrected Not Height Corrected 𝑛 2 𝑠𝑏𝑒 RM: Height Corrected: 𝜓 2 = 0.3813 Not Height Corrected: 𝜓 2 = 0.2521 12/9/2016 12

  13. 2016/10/14 Height Corrected Not Height Corrected 𝑛 2 𝑠𝑏𝑒 RM: Height Corrected: 𝜓 2 = 0.9674 Not Height Corrected: 𝜓 2 = 0.7628 12/9/2016 13

  14. 𝑂(ℎ) −1/2 exp{1 = 𝑇 ℎ 2 [1 − 𝑍 − exp(𝑍)]} 𝑂 𝑛 ℎ 1 𝑒ℎ −1 𝑍 = ℎ ℎ 𝑛 − 1 ℎ 𝑛 𝑇 ℎ ℎ 𝑛 𝑇 1 (ℎ) = 𝑑 1 sech 2 𝛾 1 1 1 𝑇 ℎ = 𝑇 1 (ℎ) + ℎ 𝑛 𝑇 2 (ℎ) 2 𝛽 ℎ ℎ 𝑛 1 + NSUMEI ET AL.: NEW VARY-CHAP TOPSIDE PROFILE (2012) 𝑇 2 (ℎ) = 𝑑 2 Data from Stephen White AFRL ℎ ℎ 𝑛 12/9/2016 14

  15. What’s happening Several Options • IGRF12 is not reporting accurate Magnetic Field • Seems unlikely due to stability of magnetic field • TEC from GPS in inaccurate • TEC compares very well to other GPS in area • Very similar to SCINDA GPS at Sevilleta • Profile is in accurate • Profile is more concentrated around Ionosphere F layer 12/9/2016 15

  16. Near Term Plans • Continue to use GPS to calibrate data for low frequency observations • Eventually, want to use GPS Corrections for correlating LWA1 and LWA Sevilleta • Can provide data universally for interested parties for VLA corrections  Updated JPL IONEX files with GPS overlay and 1min time resolution COHEN & R ̈ OTTGERING Shao, X.-M., and E. H. Lay (2016) 16 12/9/2016 16

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