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Ionosphere Observability Using GNSS and LEO Platforms Brian Breitsch Advisor: Dr. Jade Morton 1
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Page 1: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ionosphere ObservabilityUsing GNSS and LEO

Platforms

Brian BreitschAdvisor: Dr. Jade Morton

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Page 2: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Motivate ionosphere TEC observationsPast work in ionosphere observabilityObservation volume

Ground receiversLEO radio occultations (RO)Joint ground and LEO overhead/ROLEO beacons

Data affects in simulated localized imaging

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Page 3: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Image credit: NASA/J. Grobowsky 2014

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Page 4: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Image credit:

NASA

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Page 5: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

T EC = N (x)dx∫ rxsat

e

observed by multi-frequency GNSS

LEO reflection

LEO occultation

LEO beacon

ground GNSS

LEO overhead

Ionosphere TEC

low Earth-orbiting(LEO)

Global NavigationSatellite System

(GNSS)

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Page 6: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

2D and 3D ionospheremaps of electrondensity from TECmeasurements

Image Credit: "Multi-satellite ionosphere-plasmasphereelectron density reconstruction", GFZ Potsdam

Previous Work

climatological andlarge-scale

Wang Yang

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Page 7: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

"Observing System Simulation Experiment

Study on Imaging the Ionosphere by

Assimilating Observations From Ground

GNSS, LEO-Based Radio Occultation and

Ocean Reflection, and Cross Link"

PreviousWork

Xinan Yue et. al. 2013

LEO occultationslargely contribute toglobal-scale modelsdue to lack of groundRX over oceans

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Page 8: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

GNSS Ground ReceiversGPS Lab

High-rate GNSSdata collection

network

IGSStation Map

GNSS network data available

from many sources: IGS,

CORS, ARGN, etc.

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Page 9: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ground RXObservations

GNSS sky plots

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Page 10: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ground RXObservations 700 km 400 km 100 km

60°

30°

GNSS signalionosphere piercingpoints for groundreceiver atlow/mid/high latitude5° elevation mask

IPP

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Page 11: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

LEO Receiver Observations

orbital altitude: between 500-800 kmorbital inclination: 24° or 72°

occultation

tangent point (TP)

e.g. COSMIC/COSMIC-2

use POD antennahighly localized to LEOsatellite

use occultation antennastraverse large ionosphere volume

Radio Occultations (RO)

Overhead Obs.

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Page 12: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

LEO Occultations 90-day scatter of COSMIC-GPS

occultation tangent points

top coords. bottom coords.

tangent point altitude histogram

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Page 13: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

LEO Occultations

90-day histogram ofCOSMIC-GPS occultationtangent point azimuths

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Page 14: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Geometry

common observation volume

RO tangent point

Ground/LEO Common Volume

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Page 15: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

3D Line-Segment Intersection

common-volume point-of-interest

midpoint b/w points ofclosest approachGNSS rays <100 km apart

"the points of closestapproach between two line

segments"

*must handle special case where

point of closest approch is on

segment endpoint.

Ground/LEO Common Volume

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Page 16: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ground/LEOCommonVolume

60°

40°

20°

6-satellite constellation

750 km altitude

24° inclination

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Page 17: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ground/LEOCommonVolume

60°

40°

20°

6-satellite constellation

750 km altitude

72° inclination

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Page 18: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Ground/LEOCommonVolume

6-satellite constellation

750 km altitude

24° and 72° inclination

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Page 19: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

LEO BeaconObservations

LEO constellationground track coverage72° incl.

LEO beacon IPP@ 150 km and 20° elev. if we had beacon RX at every IGS station

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Page 20: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Simulated Effects onLocalized Imaging

regional IGS network inEuropelatitudes

43°-53° @ 0.25° sep.longitudes

6°-15° @ 3° sep.altitudes

100-980 km @ 20 kmattempt to reconstruct IRIimage with depletionfeature from uniformdensity starting image

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Page 21: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Simulated Effects on

Localized Imagingground

LEO RO/overhead

ground

LEO beacon

LEO RO/overhead

ground

100 km

1000 km

53°43°

no regularization used in order to emphasize affects of different

data 21

Page 22: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Future Work

Low elevation groundGNSS esspeciallyimportant at low altitudeuse 3-frequency GNSSmeasurements to addresslow-elevation TECestimation

20° el.

mask

5° el.

mask

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Page 23: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Conclusions

Poleward deficit of GNSS satellites causes gap ininformation from ground receiversOccurrence of ground and LEO GNSS observations incommon volume heavily depends upon LEO constellationorbital inclinationOverhead and RO LEO observations aid in topsideionosphere imagingLEO beacons have good potential to improve 3D imagingover ground and LEO GNSS observationsAccurate low-elevation GNSS measurements will allowimproved imaging

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Page 24: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Acknowledgements

This research was supported by the AirForce Research Laboratory and NASA.

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Page 25: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

ReferencesTS Kelso et al. Validation of sgp4 and is-gps-200d against gpsprecision ephemerides. 2007 "COSMIC-2." COSMIC 2. UCAR, n.d.http://www.cosmic.ucar.edu/cosmic2. 02 Jan. 2016.Yue, Xinan, et al. "Observing system simulation experimentstudy on imaging the ionosphere by assimilating observationsfrom ground GNSS, LEO-based radio occultation and oceanreflection, and cross link." IEEE Transactions on Geoscience andRemote Sensing 52.7 (2014): 3759-3773.Yue, Xinan, et al. "Global 3‐D ionospheric electron densityreanalysis based on multisource data assimilation." Journal ofGeophysical Research: Space Physics 117.A9 (2012).

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Page 26: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

COSMIC (LEO-based)

horizontal TP speed

proportional to vertical TP speed

proportional to∣∣v ∣∣SV

∣∣v ∣∣ cos θSV SV

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Page 27: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

images originally published at www.cosmic.ucar.edu

Occultationoccurrences over 24

hours for COSMICand COSMIC-2

COSMIC 2

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Page 28: Ionosphere Observability Using GNSS and LEO Platformsweb.stanford.edu/group/scpnt/pnt/PNT16/2016_Presentation... · 2016-11-11 · Yue, Xinan, et al. "Observing system simulation

Mask/Filters

GPS 1 (for RX) elevation > threshold(5 degrees)closest approach of LEO ray-path toEarth surface > 2 km altitude

proximity < threshold (100 km)common-volume altitude < threshold (1500 km)

Ray pathsthrough Earth

Volumes wayout in space

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