DOCSLIB.ORG

Radio Occultations Using Earth Satellites: a Wave Theory Treatment DEEP SPACE COMMUNICATIONS and NAVIGATION SERIES

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Radio Occultations Using Earth Satellites: a Wave Theory Treatment DEEP SPACE COMMUNICATIONS and NAVIGATION SERIES Radio Occultations Using Earth Satellites: A Wave Theory Treatment DEEP SPACE COMMUNICATIONS AND NAVIGATION SERIES Issued by the Deep Space Communications and Navigation Systems Center of Excellence Jet Propulsion Laboratory California Institute of Technology Joseph H. Yuen, Editor-in-Chief Previously Published Monographs in this Series 1. Radiometric Tracking Techniques for Deep-Space Navigation C. L. Thornton and J. S. Border 2. Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation Theodore D. Moyer 3. Bandwidth-Efficient Digital Modulation with Application to Deep-Space Communications Marvin K. Simon 4. Large Antennas of the Deep Space Network William A. Imbriale 5. Antenna Arraying techniques in the Deep Space Network David H. Rogstad, Alexander Mileant, and Timothy T. Pham Radio Occultations Using Earth Satellites: A Wave Theory Treatment William G. Melbourne Jet Propulsion Laboratory California Institute of Technology MONOGRAPH 6 DEEP SPACE COMMUNICATIONS AND NAVIGATION SERIES Radio Occultations Using Earth Satellites: A Wave Theory Treatment April 2004 The research described in this publication was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not constitute or imply its endorsement by the United States Government or the Jet Propulsion Laboratory, California Institute of Technology. Table of Contents Foreword..............................................................................................................xvii Preface...................................................................................................................xix Acknowledgments................................................................................................xxiii Chapter 1: Radio Occultation Using Earth Satellites Background and Overview ...........................................1 1.1 Introduction...................................................................1 1.1.1 History of the Occultation Technique ............................2 1.1.2 Occultations from Earth Satellites..................................3 1.1.3 The Global Positioning System ......................................8 1.1.4 Timing ...........................................................................11 1.1.5 Ephemerides ..................................................................12 1.2 Information Content in GPS Occultation Observations............................................................... 13 1.2.1 Connected Phase ...........................................................13 1.2.2 Sample Rate Versus Vertical Resolution .....................14 1.2.3 Inverting Radio Occultation Data.................................14 1.2.4 Assimilating Radio Occultation Data...........................17 1.2.5 Rays and Stationarity ....................................................18 1.2.6 Excess Doppler..............................................................21 1.3 Scientific Applications of GPS Occultation Observations............................................................... 23 1.3.1 Weather..........................................................................24 1.3.2 Climate...........................................................................27 1.4 Problems from Multipath and Some Remedies ......... 28 1.4.1 Spectral/Holographic Techniques.................................32 1.4.2 Back Propagation ..........................................................34 v vi 1.4.3 The Canonical Transform Technique...........................41 1.4.4 The Impact Parameter Space Curve .............................41 1.4.5 A Full-Spectrum Wave Theory ....................................43 1.5 Overview...................................................................... 47 1.5.1 Chapter 2 .......................................................................47 1.5.2 Chapter 3 .......................................................................48 1.5.3 Chapter 4 .......................................................................49 1.5.4 Chapter 5 .......................................................................50 1.5.5 Chapter 6 .......................................................................52 1.5.6 Appendices ....................................................................60 1.6 Limitations and Simplifications.................................. 61 1.6.1 Ionosphere .....................................................................61 1.6.2 Placing the Occulted GPS Satellite at Infinity .............61 1.6.3 Time...............................................................................63 1.6.4 Spherical Symmetry......................................................63 1.6.5 Coplanarity ....................................................................63 1.6.6 Circularity......................................................................64 1.6.7 Treating the GPS Signal as a Harmonic Wave ............64 1.7 Recommendations for the Next Chapters.................. 65 References ............................................................................ 66 Chapter 2: Scattering of Electromagnetic Waves from a Spherical Boundary Using a Thin Phase Screen Model and Scalar Diffraction Theory......................... 77 2.1 Introduction................................................................. 77 2.1.1 Multipath Scenarios ......................................................79 2.1.2 An Overview of Chapter 2............................................82 2.2 Geometric Optics in a Spherical Medium................... 83 2.2.1 Multipath, Shadow Zones, and Caustics According to Geometric Optics....................................86 2.2.2 Thin-Atmosphere Conditions .......................................90 Table of Contents vii 2.3 Thin Phase Screen Models ......................................... 92 2.3.1 The Helmholtz–Kirchoff Integral Theorem .................93 2.3.2 The Space Curve for Impact Parameter........................94 2.3.3 The Fresnel Phase Screen ...........................................100 2.3.4 Suitability of the Thin-Screen Model for Diffraction Analysis....................................................101 2.3.5 A Phase Profile for the Thin Screen...........................102 2.3.6 Bending-Angle Perturbations .....................................103 2.3.7 Case A: A Discontinuity in Refractivity ....................105 2.3.8 Case B: A Discontinuity in Scale Height ...................107 2.3.9 Case C: A Discontinuity in Lapse Rate......................109 2.4 Multipath Using a Thin Phase Screen Model ........... 109 2.5 Scalar Diffraction: The Rayleigh–Sommerfeld Integral ...................................................................... 114 2.6 The Stationary-Phase Technique ............................. 116 2.6.1 Necessary Conditions for Validity of the Geometric Optics Approach .......................................121 2.7 Numerical Results Using Thin-Screen/Scalar Diffraction.................................................................. 122 2.7.1 Fresnel Response to a Discontinuity in Lapse Rate ...................................................................125 2.7.2 Fresnel Response to a Discontinuity in Refractivity..................................................................128 2.7.3 A Boundary Layer.......................................................131 2.8 Sensing a Boundary in the Ionosphere.................... 133 2.8.1 Fresnel Effects at a Boundary.....................................136 2.8.2 Amplitude Effects at a Boundary ...............................139 2.8.3 Ray Splitting................................................................140 2.8.4 Doppler Information at a Boundary............................146 2.8.5 Fresnel Effects Using an Improved Electron Density Model.............................................................148 viii 2.9 The Error in the Recovered Refractivity Resulting from Fresnel Phase Perturbations ........................... 152 2.10 Fresnel Transform Techniques ............................... 156 2.10.1 Adjoining the Constraint Au()≡ 1.............................158 2.10.2 Diffraction Integral with Multipath ............................159 2.10.3 A Numerical Example.................................................159 2.10.4 Fresnel Aliasing...........................................................161 2.10.5 Numerical Results .......................................................162 References .......................................................................... 167 Chapter 3: Scattering from a Large Transparent Sphere Based on Maxwell’s Equations: Mie Scattering Theory ..................................................... 171 3.1 Introduction............................................................... 171 3.2 Scalar Potentials ....................................................... 174 3.2.1 Series Expansions for Scalar Potentials .....................176 3.3 Multiple Internal Reflections..................................... 179 3.4 Fresnel Formulas for Reflection and Transmission Amplitudes......................................... 181 3.4.1 Conservation Principle................................................184 3.4.2 Scattering Angles and Intensities ...............................185 3.4.3 Caustics........................................................................189
Load more

Recommended publications
  • Comparison Between GPS Radio Occultation and Radiosonde Sounding Data
    Comparison Between GPS Radio Occultation and Radiosonde Sounding Data Dione Rossiter Academic Affiliation, Fall 2003: Senior University of California, Berkeley SOARS® Summer 2003 Science Research Mentors: Christian Rocken, Bill Kuo, and Bill Schreiner Writing and Communications Mentor: David Gochis Community Mentor: Annette Lampert Peer Mentor: Pauline Datulayta ABSTRACT Global Positioning System (GPS) Radio Occultation (RO) is a new technique for obtaining profiles of atmospheric properties, specifically: refractivity, temperature, pressure, water vapor pressure in the neutral atmosphere, and electron density in the ionosphere. The data received from GPS RO contribute significant amounts of information to a range of fields including meteorology, climate, ionospheric research, geodesy, and gravity. Low-Earth orbiting satellites, equipped with a GPS receiver, track GPS radio signals as they set or rise behind the Earth. Since GPS signals are refracted (delayed and bent) by the Earth's atmosphere, these data are used to infer information about atmospheric refractivity. Before the GPS RO data are used for research and operations, it is essential to assess their accuracy. Therefore, this research provided quantitative estimates of the accuracy of GPS RO when compared with measurements of known accuracy. Profile statistics (mean, standard deviation, standard error) were computed as a function of altitude to quantify the errors. Comparing RO data with nearby (300km; 2hr) radiosonde data yielded small mean error for all of the statistical plots generated, affirming that the RO technique is accurate for measuring atmospheric properties. Comparison of RO data with sounding data from different radiosonde systems showed that the RO technique was of high enough accuracy to differentiate differences in performance of various types of radiosonde systems.
    [Show full text]
  • Spire's Cubesat Constellation of GNSS, AIS, and ADS-B Sensors
    Seizing Opportunity: Spire’s CubeSat Constellation of GNSS, AIS, and ADS-B Sensors Dallas Masters, Director of GNSS, Spire Global, Inc. Stanford PNT Symposium, 2018-11-08 WHO & WHAT IS SPIRE? We’re a new, innovative satellite & data services company that you might not have heard of… We’re what you get when you mix agile development with nanosatellites... We’re the transformation of a single , crowd-sourced nanosatellite into one of the largest constellations of satellites in the world... Stanford PNT Symposium, 2018-11-08 OUTLINE 1. Overview of Spire 2. Spire satellites and PNT payloads & products a. AIS ship tracking b. GNSS-based remote sensing measurements: radio occultation (RO), ionosphere electron density, bistatic radar (reflections) c. ADS-B aircraft tracking (early results) 3. Spire’s lofty long-term goals Stanford PNT Symposium, 2018-11-08 AN OVERVIEW OF SPIRE Stanford PNT Symposium, 2018-11-08 SPIRE TODAY • 150 people across five offices (a distributed start-up) - San Francisco, Boulder, Glasgow, Luxembourg, and Singapore • 60+ LEO 3U CubeSats (10x10x30 cm) in orbit with passive sensing payloads, 30+ global ground stations - 16 launch campaigns completed with seven different launch providers - Ground station network owned and operated in-house for highest level of security and resilience • Observing each point on Earth 100 times per day, everyday - Complete global coverage, including the polar regions • Deploying new applications within 6-12 month timeframes • World’s largest ship tracking constellation • World’s largest weather
    [Show full text]
  • An Observing System Simulation Experiment with a Constellation of Radio Occultation Satellites
    DECEMBER 2018 C U C U R U L L E T A L . 4247 An Observing System Simulation Experiment with a Constellation of Radio Occultation Satellites L. CUCURULL AND R. ATLAS NOAA/Atlantic Oceanographic and Meteorological Laboratory, Miami, Florida R. LI AND M. J. MUELLER Cooperative Institute for Research in the Environmental Sciences, University of Colorado Boulder, and NOAA/OAR/ESRL/Global Systems Division, Boulder, Colorado R. N. HOFFMAN Cooperative Institute for Marine and Atmospheric Studies, University of Miami, and NOAA/Atlantic Oceanographic and Meteorological Laboratory, Miami, Florida (Manuscript received 9 March 2018, in final form 17 August 2018) ABSTRACT Experiments with a global observing system simulation experiment (OSSE) system based on the recent 7-km-resolution NASA nature run (G5NR) were conducted to determine the potential value of proposed Global Navigation Satellite System (GNSS) radio occultation (RO) constellations in current operational numerical weather prediction systems. The RO observations were simulated with the geographic sampling expected from the original planned Constellation Observing System for Meteorology, Ionosphere, and Climate-2 (COSMIC-2) system, with six equatorial (total of ;6000 soundings per day) and six polar (total of ;6000 soundings per day) receiver satellites. The experiments also accounted for the expected improved vertical coverage provided by the Jet Propulsion Laboratory RO receivers on board COSMIC-2. Except that RO observations were simulated and assimilated as refractivities, the 2015 version of the NCEP’s operational data assimilation system was used to run the OSSEs. The OSSEs quantified the impact of RO observations on global weather analyses and forecasts and the impact of adding explicit errors to the simulation of perfect RO profiles.
    [Show full text]
  • An Introduction to GPS Radio Occultation and Its Use in NWP
    An introduction to GPS radio occultation and its use in NWP John Eyre Met Office, UK GRAS SAF Workshop on “Applications of GPS radio occultation measurements“; © Crown copyright 2007 ECMWF; 16-18 June 2008 An introduction to GPS radio occultation and its use in NWP • Radio occultation (RO) – introduction • Variational data assimilation – introduction • Assimilation options for RO data • Some issues for this Workshop © Crown copyright 2007 GPS – the source data The Global Positioning System (GPS) • multi-purpose - applications in positioning, navigation, surveying, … • nominal GPS network = 24 satellites • near polar orbit - height ~20000 km • allows high-accuracy positioning of low Earth orbiters (LEOs) • source of refracted radio signals for radio occultation © Crown copyright 2007 Geometry of a radio occultation measurement Tangent point Bending angle α LEO a GPS Impact parameter © Crown copyright 2007 An occultation sounded region receiver transmitter Earth atmosphere A sounding from 60 km to the surface takes ~60s © Crown copyright 2007 Atmospheric refraction: the physics Refractivity gradients caused by gradients in: • density (pressure and temperature) • water vapour • electron density • (liquid water) 2 2 N = κ1 p / T + κ2 e / T + κ3 ne / f + κ4 W “dry” “moist” ionosphere “scattering” N = refractivity = (n -1) x 106 n = refractive index p = pressure T = temperature e = water vapour pressure ne = electron density f = frequency W = liquid water density © Crown copyright 2007 From bending angle to density Impact parameter Bending angle LEO GPS L1: 1.575 GHz / 19.0 cm L2: 1.227 GHz / 24.4 cm 1(')∞ α a pe ln(na ( ))= da ' 6 ∫a 22 Nn=−×(1)10 =κκ12 + π aa' − T T 2 Refractive index Refractivity © Crown copyright 2007 Features of RO measurements • globally distributed • temperature in stratosphere and upper troposphere, and ..
    [Show full text]
  • An Investigation of GNSS Radio Occultation Atmospheric Sounding
    An Investigation of GNSS Radio Occultation Atmospheric Sounding Technique for Australian Meteorology A thesis submitted in fulfilment of the requirements for the degree of Doctor of Philosophy Erjiang Fu B.S. School of Mathematical and Geospatial Sciences College of Science, Engineering and Health RMIT University August 2011 I (This page intentionally left blank) II Declaration I certify that except where due acknowledgement has been made, the work is that of the author alone; the work has not been submitted previously, in whole or in part, to qualify for any other academic award; the content of the thesis is the result of work which has been carried out since the official commencement date of the approved research program; any editorial work, paid or unpaid, carried out by a third party is acknowledged; and, ethics procedures and guidelines have been followed. Erjiang Fu I (This page intentionally left blank) II Acknowledgements First of all, I would like to thank my supervisors: Professor Kefei Zhang, Dr David Silcock and Dr Yuriy Kuleshov. This thesis would not have been possible without their inspiration, guidance, support and encouragement in the past four years. Especially, my main supervisor Professor Zhang, also one of my close friends, who opened the door of a scientific career for me. During the research journey, it was my greatest honour to work with many respectable scientists and researchers. Sincere thanks go to Professor Yuei-An Liou, Professor Alexander Pavelyev, Dr Xiaolan Wang, Dr Kaye Marion, Dr Suqin Wu, Dr Chuan-Sheng Wang, Dr Robert Norman, Dr Gang-Jun Liu, Dr Falin Wu, Dr Xiaohua Xu, Dr Sue Choy, Dr Xinjia Zhou, Dr Yan Wang, Dr Dongju Peng, Dr Ming Zhu, Mr Bobby Wong, Mr Toby Manning, Miss Ying Li, Ms Jing Peng, Mr Stuart Whitman, Mr Alex Chen, Miss Gap Vimvipa, and others.
    [Show full text]
  • An Analysis Study of FORMOSAT-7/COSMIC-2 Radio Occultation Data in the Troposphere
    remote sensing Article An Analysis Study of FORMOSAT-7/COSMIC-2 Radio Occultation Data in the Troposphere Shu-Ya Chen 1 , Chian-Yi Liu 1,2,3,* , Ching-Yuang Huang 1,3, Shen-Cha Hsu 3, Hsiu-Wen Li 1, Po-Hsiung Lin 4, Jia-Ping Cheng 5 and Cheng-Yung Huang 6 1 GPS Science and Application Research Center, National Central University, Taoyuan 32001, Taiwan; [email protected] (S.-Y.C.); [email protected] (C.-Y.H.); [email protected] (H.-W.L.) 2 Center for Space and Remote Sensing Research, National Central University, Taoyuan 32001, Taiwan 3 Department of Atmospheric Sciences, National Central University, Taoyuan 32001, Taiwan; [email protected] 4 Department of Atmospheric Sciences, National Taiwan University, Taipei 10617, Taiwan; [email protected] 5 Central Weather Bureau, Taipei 10048, Taiwan; [email protected] 6 National Space Organization, National Applied Research Laboratories, Hsinchu 30078, Taiwan; [email protected] * Correspondence: [email protected]; Tel.: +886-3-4227151 (ext. 57618) Abstract: This study investigates the Global Navigation Satellite System (GNSS) radio occultation (RO) data from FORMOSAT-7/COSMIC-2 (FS7/C2), which provides considerably more and deeper profiles at lower latitudes than those from the former FORMOSAT-3/COSMIC (FS3/C). The statistical analysis of six-month RO data shows that the rate of penetration depth below 1 km height within ±45◦ latitudes can reach 80% for FS7/C2, significantly higher than 40% for FS3/C. For verification, FS7/C2 RO data are compared with the observations from chartered missions that provided aircraft dropsondes and on-board radiosondes, with closer observation times and distances from the oceanic Citation: Chen, S.-Y.; Liu, C.-Y.; RO occultation over the South China Sea and near a typhoon circulation region.
    [Show full text]
  • 2.3 CONSTELLATION OBSERVING SYSTEM for METEOROLOGY IONOSPHERE and CLIMATE (COSMIC): an OVERVIEW Ying-Hwa Kuo*, Christian Rocke
    2.3 CONSTELLATION OBSERVING SYSTEM FOR METEOROLOGY IONOSPHERE AND CLIMATE (COSMIC): AN OVERVIEW Ying-Hwa Kuo*, Christian Rocken, and Richard A. Anthes University Corporation for Atmospheric Research, Boulder, CO, U.S.A. 1. INTRODUCTION The GPS RO sounding technique, making use of highly coherent radio signals from the GPS has The Global Positioning System (GPS) satellite many unique characteristics, including: (i) high constellation was developed for precise navigation accuracy, (ii) high vertical resolution, (iii) all and positioning. The GPS today consists of 28 weather sounding capability, (iv) independent of operational satellites that transmit L-band radio radiosonde or other calibration, (v) no instrument signals at two frequencies (L1 at 1.57542 GHz and drift and (vi) no satellite-to-satellite bias (Rocken et L2 at 1.2276 GHz) to a wide variety of users in al. 1997; Kursinski et al. 1997; Kuo et al. 2004). navigation, time transfer, and relative positioning These characteristics make GPS RO data ideally and for an ever-increasing number of scientists in suited for climate monitoring and global weather geodesy, atmospheric sciences, oceanography, prediction. Anthes et al. (2000) provided many and hydrology. examples on the possible applications of GPS RO Atmospheric soundings are obtained using data to meteorology and climate. GPS through the radio occultation (RO) technique, in which satellites in low-Earth orbit (LEO), as they 2. BRIEF DESCRIPTION OF THE COSMIC rise and set relative to the GPS satellites, measure MISSION the phase of the GPS dual-frequency signals. From this phase the Doppler frequency is COSMIC (Constellation Observing System for computed. The Doppler shifted frequency Meteorology, Ionosphere and Climate) is a joint measurements are used to compute the bending mission between Taiwan and U.S., with a goal to angles of the radio waves, which are a function of demonstrate the use of GPS RO data in atmospheric refractivity.
    [Show full text]
  • Extending the Global Mass Change Data Record: GRACE Follow‐On Instrument and Science Data Performance
    Originally published as: Landerer, F. W., Flechtner, F., Save, H., Webb, F. H., Bandikova, T., Bertiger, W. I., Bettadpur, S. V., Byun, S., Dahle, C., Dobslaw, H., Fahnestock, E., Harvey, N., Kang, Z., Kruizinga, G. L. H., Loomis, B. D., McCullough, C., Murböck, M., Nagel, P., Paik, M., Pie, N., Poole, S., Strekalov, D., Tamisiea, M. E., Wang, F., Watkins, M. M., Wen, H., Wiese, D. N., Yuan, D. (2020): Extending the global mass change data record: GRACE Follow‐On instrument and science data performance. ‐ Geophysical Research Letters, 47, 12, e2020GL088306. https://doi.org/10.1029/2020GL088306 RESEARCH LETTER Extending the Global Mass Change Data Record: GRACE 10.1029/2020GL088306 Follow‐On Instrument and Science Data Performance Key Points: Felix W. Landerer1 , Frank M. Flechtner2,5 , Himanshu Save3 , Frank H. Webb1, • GRACE‐FO is extending the 15‐year 1 1 3 1 GRACE record of global monthly Tamara Bandikova , William I. Bertiger , Srinivas V. Bettadpur , Sung Hun Byun , mass change at an equivalent Christoph Dahle2 , Henryk Dobslaw2 , Eugene Fahnestock1, Nate Harvey1, Zhigui Kang3, precision and spatiotemporal Gerhard L. H. Kruizinga1, Bryant D. Loomis4 , Christopher McCullough1 , sampling 2,5 3 1 3 3 • Since its launch in 2018, GRACE‐FO Michael Murböck , Peter Nagel , Meegyeong Paik , Nadege Pie , Steve Poole , has observed large water storage and Dmitry Strekalov1, Mark E. Tamisiea3, Furun Wang3, Michael M. Watkins1, Hui‐Ying Wen1, ice mass changes driven by David N. Wiese1 , and Dah‐Ning Yuan1 interannual climate anomalies • GRACE‐FO's instrument/flight 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA, 2Helmholtz Centre Potsdam GFZ system performance has largely 3 improved over GRACE.
    [Show full text]
  • Radio Occultation Activities at NASA CGMS-39 White Paper, October 2011 A
    Radio Occultation Activities At NASA CGMS-39 White Paper, October 2011 A. J. Mannucci1, T. K. Meehan1, B. A. Iijima1, L. E. Young1, G. Franklin1, L. Cucurull2 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 2 NOAA/NWS/NCEP/EMC, Washington, DC 1. Overview NASA/JPL has been involved in radio occultation science since its early demonstration and development on planetary missions in the 1970s. NASA modified a TurboRogue geodetic GPS receiver to create the first GPS radio occultation instrument for the GPS/MET proof of concept mission in 1995. National Science Foundation and University Corporation For Atmospheric Research (UCAR) were partners on GPS/MET. The initial atmospheric profiles obtained in 1995 were successful, leading to follow-on development and mission deployment. GPS/MET provided valuable information for NASA to develop a dedicated GPS radio occultation (RO) instrument, the “BlackJack.” The BlackJack design is the basis for operational assimilation of RO data on the following missions: COSMIC, CHAMP, SAC- C, C/NOFS, GRACE, and TerraSAR-X. The BlackJack instrument successfully demonstrated the following technologies: 1) 24/7 tracking – overcoming GPS signal encryption GPS/MET dual-frequency tracking only occurred during a few 2-week periods when GPS signal encryption was intentionally disabled. The BlackJack design is capable of continuously tracking two GPS frequencies, as needed for operations. 2) Doubling data volume – rising occultations Acquiring occultations from a forward viewing antenna doubles the quantity of data from a single instrument, at the cost of an additional antenna input and increased processing load on the instrument. 3) Mid-to-lower troposphere data – open loop tracking Tracking the signal dynamics using predicts rather than tracking loop feedback enables improved data quality where the signal dynamics is highest: in the mid to lower troposphere (below ~8 km altitude).
    [Show full text]
  • GNSS Radio Occultation Constellation Observing System Experiments
    692 GNSS radio occultation constellation observing system experiments Peter Bauer, Gabor´ Radnoti,´ Sean Healy, Carla Cardinali Research Department Submitted to Monthly Weather Review February 2013 Series: ECMWF Technical Memoranda A full list of ECMWF Publications can be found on our web site under: http://www.ecmwf.int/publications/ Contact: [email protected] c Copyright 2013 European Centre for Medium-Range Weather Forecasts Shinfield Park, Reading, RG2 9AX, England Literary and scientific copyrights belong to ECMWF and are reserved in all countries. This publication is not to be reprinted or translated in whole or in part without the written permission of the Director- General. Appropriate non-commercial use will normally be granted under the condition that reference is made to ECMWF. The information within this publication is given in good faith and considered to be true, but ECMWF accepts no liability for error, omission and for loss or damage arising from its use. GNSS radio occultation constellation observing system experiments Abstract Observing system experiments within the operational ECMWF data assimilation framework have been performed for summer 2008 when the largest recorded number of GNSS radio occultation ob- servations from both operational and experimental satellites has been available. Constellations with 0, 5, 33, 67, and 100% data volume were assimilated to quantify the sensitivity of analysis and forecast quality to radio occultation data volume. These observations mostly constrain upper tropo- spheric and stratospheric temperatures and correct an apparent model bias that changes sign across the upper troposphere - lower stratosphere. This correction effect does not saturate with increasing data volume, even if more data is assimilated than available in today’s analyses.
    [Show full text]
  • Accuracy Assessment of the Quiet-Time Ionospheric F2 Peak Parameters As Derived from COSMIC-2 Multi-GNSS Radio Occultation Measurements
    J. Space Weather Space Clim. 2021, 11,18 Ó I. Cherniak et al., Published by EDP Sciences 2021 https://doi.org/10.1051/swsc/2020080 Available online at: www.swsc-journal.org Topical Issue - Space Weather Instrumentation TECHNICAL ARTICLE OPEN ACCESS Accuracy assessment of the quiet-time ionospheric F2 peak parameters as derived from COSMIC-2 multi-GNSS radio occultation measurements Iurii Cherniak1,*, Irina Zakharenkova1, John Braun1, Qian Wu1,2, Nicholas Pedatella1,2, William Schreiner1, Jan-Peter Weiss1, and Douglas Hunt1 1 COSMIC Program Office, University Corporation for Atmospheric Research, Boulder, CO 80301, USA 2 High Altitude Observatory, National Center for Atmospheric Research, Boulder, CO 80301, USA Received 30 June 2020 / Accepted 24 December 2020 Abstract – The Constellation Observing System for Meteorology, Ionosphere, and Climate 2 (COSMIC-2) mission was launched into a low-inclination (24°) orbit on June 25, 2019. Six satellites, each with an advanced Tri-GNSS Radio-Occultation Receiver System (TGRS), provide a global and uniform data coverage of the equatorial region with several thousand electron density profiles daily. The COSMIC-2 electron density profiles, and specifically the derived ionospheric F2 peak parameters, are properly validated in this study with reliable “truth” observations. For this purpose, we used manually scaled ionograms from 29 ground-based ionosondes located globally at low and middle latitudes. For this valida- tion campaign, we considered only geomagnetically quiet conditions in order to establish benchmark level of the new mission’s ionospheric observation quality and to evaluate the operational capability of the COSMIC-2 Radio Occultation (RO) payload at the background of normal day-to-day variability of the ionosphere.
    [Show full text]
  • Radio Science
    CASSINI RADIO SCIENCE 1, 1 1 1 A. J. KLIORE ∗,J.D. ANDERSON ,J.W. ARMSTRONG ,S.W. ASMAR , C. L. HAMILTON1,N.J. RAPPAPORT1,H.D.WAHLQUIST1,R. AMBROSINI2, F. M. FLASAR3,R.G. FRENCH4,L. IESS5, E. A. MAROUF6 and A. F. NAGY7 1JetPropulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109, USA 2Istituto di Radioastronomia CNR, Via Gobetti 101, I-40129, Bologna, Italy 3NASA-Goddard Space Flight Center, Greenbelt, MD 20771, USA 4Wellesley College, Wellesley, MA 02481, USA 5Universitad` i Roma ‘La Sapienza’, Via Eudossiana 18, I-00184 Roma, Italy 6San Jose State University, One Washington Square, San Jose, CA 95192, USA 7University of Michigan, 2455 Hayward Avenue, Ann Arbor, MI 48109, USA (∗author for correspondence, e-mail: [email protected]) (Received 29 December 1999; Accepted in final form 4 April 2002) Abstract. Cassini radio science investigations will be conducted both during the cruise (gravitational wave and conjunction experiments) and the Saturnian tour of the mission (atmospheric and ionospheric occultations, ring occultations, determinations of masses and gravity fields). New technologies in the construction of the instrument, which consists of a portion on-board the spacecraft and another portion on the ground, including the use of the Ka-band signal in addition to that of the S- and X-bands, open opportunities for important discoveries in each of the above scientific areas, due to increased accuracy, resolution, sensitivity, and dynamic range. Keywords: atmospheres, Cassini, gravitational fields, gravitational waves, general relativity, iono- spheres, occultations, planetary rings, radio science, Saturn, Titan 1. Introduction This paper, produced by the Cassini Radio Science Team during the early cruise of the Cassini spacecraft en route for the Saturnian system, records major reference information concerning the investigations to be conducted, and the instrument that will be operated to conduct these investigations.
    [Show full text]