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May 12-14, 2015 1 Recent Developments in Understanding Natural-Hazards-Generated TEC Perturbations: Measurements and Modeling Results 1 Jet Propulsion Laboratory California Institute of Technology M/S 138-300 4800 Oak Grove Drive Pasadena CA 91109 Email: [email protected] Komjathy 1 A., Y-M. Yang 1 , X, Meng 1 , E. Shume 1 , O. Verkhoglyadova 1 , A.J. Mannucci 1 and R.B. Langley 2 IES 2015, Alexandria, Virginia 2 University of New Brunswick Fredericton, NB Canada

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  • May 12-14, 2015 1

    Recent Developments in Understanding Natural-Hazards-Generated TEC

    Perturbations: Measurements and Modeling Results

    1Jet Propulsion Laboratory California Institute of Technology

    M/S 138-300 4800 Oak Grove Drive Pasadena CA 91109

    Email: [email protected]

    Komjathy1 A., Y-M. Yang1, X, Meng1, E. Shume1, O. Verkhoglyadova1, A.J. Mannucci1

    and R.B. Langley2

    IES 2015, Alexandria, Virginia

    2University of New Brunswick Fredericton, NB Canada

    mailto:[email protected]

  • May 12-14, 2015 2

    Introduction

    Natural hazards generate waves in the thermosphere and ionosphere that may be detected using ground and space-based GPS observations.

    There is an abundance of current and future GNSS signals that we can use in a real-time and post-processing modes.

    Our objective has been to use GNSS ground-based and space-based GPS measurements to develop new technologies for e.g., augmenting natural hazards early warning systems.

    Our goal is improved understanding of wave propagation properties, acoustic and gravity wave velocities, directions, etc.

    Physics-based modeling and observational evidence. Differentiate between disturbances generated in situ versus those

    arising from natural hazards. Recent examples of ionospheric disturbances generated by:

    Earthquakes and tsunamis using ground-based and space-based GPS data,

    High-latitude plasma irregularities using high-rate RO measurements

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 3 IES 2015, Alexandria, Virginia

    Tohoku-Oki Tsunami, March 11, 2011

    Magnitude 9.0 70 km off shore 30 km depth Tsunami wave heights

    up to 15 meters

    Nepal (Gorkha) Mw 7.8 Earthquake on Apr 25,

    2015

    Our Motivation and Constant Reminders to Improve Our Understanding of Natural Hazards

  • May 12-14, 2015 4

    IGS Network

    Altitude

    F - region

    Electron Densities

    Tsunami Waves

    Ionospheric disturbances

    Tsunami-Driven Traveling Ionospheric Disturbances (TIDs)

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 5

    Earthquake: 05:46:23 UT

    Tohoku Tsunami Seen in Ionosphere Using GPS Data Compared with JPLs Tsunami Model

    One of 1200 GPS receiver observations

    Earthquakes and tsunamis generate atmospheric gravity waves that propagate vertically, reaching the ionosphere.

    Disturbance to ionosphere is detectable using

    GPS-derived total electron content (TEC).

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 6

    IPPs from Simulated Constellations by 2025

    Six different satellite constellations by 2015: GPS GLONASS Galileo BeiDou QZSS IRNSS

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 7 IES 2015, Alexandria, Virginia

    What would be the impact if the1964 Mw 9.2 earthquake were to hit the US today?

    Movie to play

  • May 12-14, 2015 8

    GPS + GLONASS data processed, all satellites utilized and plotted

    1-sec data analyzed filtered for acoustic waves

    Nepal Mw 7.8 Earthquake Ionosphere Response on April 25

    IES 2015, Alexandria, Virginia

    1-sec PPP solution at LHAZ

    Surface displacement at 10 cm level

  • May 12-14, 2015 9

    IGS site LHAZ is located about 650 km from the EQ epicenter

    It takes about 8 minutes for acoustic waves to reach the ionosphere and about 13 minutes to travel 650 km (wave velocity is ~800 m/s at 350 km)

    Ear

    thqu

    ake

    Tim

    e

    8 + 13 minutes

    Nepal Mw 7.8 Earthquake Ionosphere Response on April 25

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 10 IES 2015, Alexandria, Virginia

    Nepal Mw 7.8 Earthquake Ionosphere Response on April 25

    High-rate: 0.2 sec data

    High-rate 0.2 sec data

    15 sec data

  • May 12-14, 2015 11

    Space-Based Detection Capabilities

    IES 2015, Alexandria, Virginia

    GRACE Mission

  • May 12-14, 2015 12

    Space-Based Natural Hazards Remote Sensing in the Ionosphere

    Image Credit: European Space Agency

    GRACE B

    GRACE A

    GRACE very-high-precision inter-satellite measurements are used for: detecting ionospheric TEC perturbations, retrieving neutral air density perturbations and analyzing ionospheric and atmospheric perturbations and interpretation

    Phase advance:

    Relative accelerations:

    Comparisons with ground-based measurements, which include: GPS, seismic, and infrasound data

    IES 2015, Alexandria, Virginia

    Observation Equations:

    GRACE B

    GPS

  • May 12-14, 2015 13

    Space-Based TEC Observations

    IES 2015, Alexandria, Virginia

    GRACE ground tracks at event time

    GRACE ground tracks after/ before event time

    4 mins

    2 mins

    S-wave

    P-wave

    wavelet spectrum

    TEC perturbations

    Period

    Time after main shock [min]

    Freq

    uenc

    y [m

    Hz]

  • May 12-14, 2015 14

    Space-Based Neutral Air Density Observations

    IES 2015, Alexandria, Virginia

    GRACE observations

    Coherence Spectrum Coherence Values (Unitless)

    GITM simulations

    4 mins

    2 mins

  • May 12-14, 2015 15

    CASSIOPE Satellite GAP Observations

    CASSIOPE is a multi-task Canadian satellite which was to launched into a high inclination orbit in September 2013

    GAP-A antennas (4): high precision navigation and attitude determination (mounted on zenith-facing side)

    GAP-O antenna (1): occultation (mounted on the anti-ram side)

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 16

    Phase Scintillation Using RO Data

    At higher H , is getting smaller as the irregularities length scales get smaller and less varied

    IES 2015, Alexandria, Virginia

    Auroral oval max 16 cm; Polar cap max 3 cm

    Strong phase scintillations > 12cm in the E region & F region < 600 km

  • May 12-14, 2015 17

    Six-satellite COSMIC constellation Launched April 14, 2006

    Low-Earth Orbiter GPS

    Electron Density Profile

    COSMIC Ionospheric Weather Constellation

    IES 2015, Alexandria, Virginia

    Space COSMIC Radio Occultation, DMSP SSUSI

    DORIS proposed for COSMIC-2 Polar

  • May 12-14, 2015 18

    GNSS Receiver Payload and COSMIC-2/FORMOSAT-7

    TriG GNSS Radio Occultation System TGRS-Reflections and DORIS (RAD) Equatorial/6 Sats/Launch 2016 Polar/6 Sats/Launch 2018

    65 W avg power

    Optional

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 19

    CubeSat for Natural-Hazard Estimation With Ionospheric Sciences (CNEWS)

    IES 2015, Alexandria, Virginia

    Total Electron Content (TEC) uncertainty: 0.02 TECU

    Sensitivity estimates of geomagnetic field and TEC after de-dispersion of HF/VHF; Geomagnetic field measurements uncertainty: 50 nT

  • May 12-14, 2015 20

    Conclusions New space-physics applications using ground-based or space-based GPS

    data include investigations of: Various natural hazards that may be observed using TEC data from

    ground and space-based GPS observations. Tsunamis, earthquakes, volcanic eruptions, meteor impacts, industrial

    explosions generating atmospheric waves that we can use to learn about wave propagation properties.

    Using NASAs real-time ground-based GDGPS system and RO data to observe natural hazards to augment existing tsunami early warning systems.

    Irregularity scales and phase scintillation characteristics as functions of the solar wind and magnetospheric forcing.

    Large length scales and more intense phase scintillations are prevalent in the auroral oval compared to the polar cap.

    Space climate and real-time space weather applications using data assimilation

    NASA HQ and NASA ROSES Grant (NNH07ZDA001N-ESI) are gratefully acknowledged.

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 21

    BACKUP SLIDES

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 22

    GITM Modeling and Simulations

    Presented at the ION Pacific PNT Meeting

    Movie to play

  • May 12-14, 2015 23

    Absolute (Calibrated) and Relative COSMIC and C/NOFS TEC Data for Nov 21, 2008

    IES 2015, Alexandria, Virginia

    Bias-removed absolute C/NOFS slant TEC data

    C/NOFS relative slant TEC data

    Bias-removed absolute COSMIC slant TEC data

    COSMIC relative slant TEC data

  • May 12-14, 2015 24

    Nowcasts Multi-Resolution and Multiple Data Sets

    IES 2015, Alexandria, Virginia

    GAIM: Global electron density grids continuously updated

    Ground-based: GPS TEC

    Space COSMIC Radio Occultation, DMSP SSUSI

    DORIS proposed for COSMIC-2 Polar

    + Ionosonde global

    network

    Nested grid GAIM High resolution locally

    Tomographic inversion of GUVI/SSUSI data

    Comberiate et al., GRL 2006

  • May 12-14, 2015 25

    Real-Time GAIM TEC Residuals for Tohoku Earthquake on March 11, 2011

    GIM residuals (a) and band-pass filtered slant TEC measurements. Panel (b) indicates an example for filtered TEC observations.

    NASAs GDGPS R&D role is highly valuable and gratefully acknowledged

    IES 2015, Alexandria, Virginia

    GAIM: Global Assimilative Ionosphere Model GIM: Global Ionospheric (TEC) Maps

  • May 12-14, 2015 26 IES 2015, Alexandria, Virginia

    Arecibo

    FM2

    FM5 GPS15

    20:05 20:09

    20:21

    20:25

    CRO1 JAMA

    SCUB CRO1

    UT 20:00

    Arecibo ISR Case Study for June 26, 2006

    UT 20:00

    UT 20:12 UT 20:24

  • May 12-14, 2015 27

    Ground-Based GPS, COSMIC and Jicamarca ISR Coverage for Sept 21, 2014

    Ground GPS COSMIC

    Jicamarca ISR dense but unevenly distributed coverage

    less dense yet evenly distributed coverage

    IES 2015, Alexandria, Virginia

  • May 12-14, 2015 28 IES 2015, Alexandria, Virginia

    An Example of COSMIC Impact on Profile Shape

    2. UT 15:48

    3. UT 16:36 COSMIC UT 15:30

    UT hours

    1. UT 15:24

    1. 2. 3.

    1. UT 15:36

    Komjathy1 A., Y-M. Yang1, X, Meng1, E. Shume1, O. Verkhoglyadova1, A.J. Mannucci1 and R.B. Langley2IntroductionSlide Number 3Slide Number 4Tohoku Tsunami Seen in Ionosphere Using GPS Data Compared with JPLs Tsunami ModelSlide Number 6Slide Number 7Slide Number 8Slide Number 9Nepal Mw 7.8 Earthquake Ionosphere Responseon April 25Space-Based Detection CapabilitiesSpace-Based Natural Hazards Remote Sensingin the Ionosphere Space-Based TEC ObservationsSpace-Based Neutral Air Density ObservationsCASSIOPE Satellite GAP Observations Phase Scintillation Using RO DataSlide Number 17GNSS Receiver Payload and COSMIC-2/FORMOSAT-7CubeSat for Natural-Hazard Estimation With Ionospheric Sciences (CNEWS) ConclusionsSlide Number 21GITM Modeling and SimulationsAbsolute (Calibrated) and Relative COSMIC and C/NOFS TEC Data for Nov 21, 2008Nowcasts Multi-Resolution and Multiple Data SetsReal-Time GAIM TEC Residualsfor Tohoku Earthquake on March 11, 2011Slide Number 26Slide Number 27An Example of COSMIC Impact on Profile Shape