On the application of meteorological data assimilation techniques to radio occultation measurements of the ionosphere Matthew Angling Centre for RF Propagation and Atmospheric Research www.QinetiQ.com © Copyright QinetiQ limited 2006 Ionospheric data assimilation • To provide a high accuracy and timely specification of the ionosphere for use in RF systems • Increased accuracy of ground and space based trans-ionospheric sensors − EWR, SAR, AMTI/GMTI, satellite geolocation systems • Improved accuracy of single frequency navigation systems − GPS, Galileo • Improved LPI/LPJ characteristics of HF communications • Significant reduction in the errors for HF position finding systems www.QinetiQ.com © Copyright QinetiQ limited 2006 2 Estimation LT persistence Forecast Empirical •IRI •RIBG •PIM Shells •Single •Multiple Non-optimal •Profile adjustment •Tomography •ART, MART, etc Physical •Ionospheric •Coupled 3D basis functions •Horiz harmonics •Vertical EOFs 3D grid •Geographic •Geomagnetic Optimal •DIT •GMKF •Approx Kalman •Full Kalman •Variational methods covariances Representation No covariances Model Physical forecast Data assimilation models www.QinetiQ.com © Copyright QinetiQ limited 2006 3 Estimation LT persistence Forecast Empirical •IRI •RIBG •PIM Shells •Single •Multiple Non-optimal •Profile adjustment •Tomography •ART, MART, etc Physical •Ionospheric •Coupled 3D basis functions •Horiz harmonics •Vertical EOFs 3D grid •Geographic •Geomagnetic Optimal •DIT •GMKF •Approx Kalman •Full Kalman •Variational methods covariances Representation No covariances Model Physical forecast JPL GIM www.QinetiQ.com © Copyright QinetiQ limited 2006 4 Estimation LT persistence Forecast Empirical •IRI •RIBG •PIM Shells •Single •Multiple Non-optimal •Profile adjustment •Tomography •ART, MART, etc Physical •Ionospheric •Coupled 3D basis functions •Horiz harmonics •Vertical EOFs 3D grid •Geographic •Geomagnetic Optimal •DIT •GMKF •Approx Kalman •Full Kalman •Variational methods covariances Representation No covariances Model Physical forecast IonoNumerics www.QinetiQ.com © Copyright QinetiQ limited 2006 5 Estimation LT persistence Forecast Empirical •IRI •RIBG •PIM Shells •Single •Multiple Non-optimal •Profile adjustment •Tomography •ART, MART, etc Physical •Ionospheric •Coupled 3D basis functions •Horiz harmonics •Vertical EOFs 3D grid •Geographic •Geomagnetic Optimal •DIT •GMKF •Approx Kalman •Full Kalman •Variational methods covariances Representation No covariances Model Physical forecast USU GAIM www.QinetiQ.com © Copyright QinetiQ limited 2006 6 Estimation LT persistence Forecast Empirical •IRI •RIBG •PIM Shells •Single •Multiple Non-optimal •Profile adjustment •Tomography •ART, MART, etc Physical •Ionospheric •Coupled 3D basis functions •Horiz harmonics •Vertical EOFs 3D grid •Geographic •Geomagnetic Optimal •DIT •GMKF •Approx Kalman •Full Kalman •Variational methods covariances Representation No covariances Model Physical forecast Electron Density Assimilative Model www.QinetiQ.com © Copyright QinetiQ limited 2006 7 Electron Density Assimilative Model • PIM used for background model − Electrons only • Designed to be scalable − Can assimilate single or multiple measurements • Low demands on computer resources • Simple evolution − Exponential decay of electron density grid differences • Uses sun-fixed geomagnetic coordinate system • Model Variances are propagated, covariance are estimated as required www.QinetiQ.com © Copyright QinetiQ limited 2006 8 Best Linear Unbiased Estimator Most probable atmospheric state (xa) is obtained by modifying background state (xb) with differences between the observation vector (y) and the background state xa xb K(y Hx b ) K BH HBH R T T 1 xa = most probable atmospheric state xb = a priori (background) atmospheric model y = observations B = background error covariance matrix H = observation operator R = observation error covariance matrix K = weight matrix www.QinetiQ.com © Copyright QinetiQ limited 2006 9 www.QinetiQ.com © Copyright QinetiQ limited 2006 10 Radio Occultation • GPS transmitter, LEO receiver vGPS • Global coverage with high vertical, low horizontal resolution βGPS GPS φGPS • In the ionosphere bending angles are small • Estimating slant TEC from L1/L2 phase difference removes clock and POD errors rGPS a r • Assimilation of sTEC has v potential to overcome limitations of Abel Transform lEO • RO provides important height information a βLEO φLEO rlEO Earth LEO www.QinetiQ.com © Copyright QinetiQ limited 2006 11 foF2/hmF2 testing • Previous study has shown that EDAM can improved foF2 performance • But hmF2 performance is relatively poor • Can RO data improve representation of vertical structure in EDAM? www.QinetiQ.com © Copyright QinetiQ limited 2006 12 Assimilation tests • Assimilations run for 19-20 August and 4, 10 September 2006 − Disturbed, moderate and quiet conditions • Assimilate COSMIC podTEC data − Calibrated slant TEC − Reduced sampling rate at high elevations − Constellation is not yet fully deployed • Runs with just RO data, just IGS data and with RO + IGS data • Test using vertical profiles − ionPRF files from UCAR-CDAAC − Abel Transform vertical profiles − True height profiles from AFRL vertical ionosonde network www.QinetiQ.com © Copyright QinetiQ limited 2006 13 IGS and DISS stations www.QinetiQ.com © Copyright QinetiQ limited 2006 14 Example ionPRF vertical profile • RMS error in electron density calculated at 4 km intervals • Little quality control of ionPRF − Values must be positive • Not comparing similar measurements − ionPRF is a distributed measurement www.QinetiQ.com © Copyright QinetiQ limited 2006 15 IonPRF RMS errors www.QinetiQ.com © Copyright QinetiQ limited 2006 16 IonPRF RMS errors www.QinetiQ.com © Copyright QinetiQ limited 2006 17 Example VI vertical profile • RMS error in electron density calculated at 4 km intervals • Little quality control of VI profile − Autoscaled data − Values must be positive • No attempt to limit VI data to that close to RO measurements www.QinetiQ.com © Copyright QinetiQ limited 2006 18 VI RMS errors www.QinetiQ.com © Copyright QinetiQ limited 2006 19 VI RMS errors www.QinetiQ.com © Copyright QinetiQ limited 2006 20 Conclusions • COSMIC podTEC data has a positive effect on EDAM analysis • For moderate and disturbed conditions, assimilation of podTEC improves the electron density RMS error at all heights from 200 to 500 km • The interaction between podTEC and ground based TEC requires further investigation • Modest improvements, limited by − Difficult test − COSMIC constellation − Autoscaled vertical ionosonde data www.QinetiQ.com © Copyright QinetiQ limited 2006 21
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