Height System Unificationand GOCE. Reiner Rummel, Michael Sideris, Phil Woodworth

Similar documents
Along track profiles of dynamic ocean topography as an essential tool for the improvement of Brazilian heights

Who am I? National Geodetic Survey s Great Lakes Region Geodetic Advisor. John Ellingson Cell:

Notes on the History of the National Geodetic Vertical Datum 1929 and the North American Vertical Datum 1988 in Alaska, U.S.A. 1

Discussion of the leveling network geometry needed for the SIRGAS vertical reference system realization

Data Origination, Management and WGS 84. ICAO PBN Seminar Data Origination & Management and WGS 84

ACES Atomic Clock Ensemble in Space

$6.60 NEW SOUTH WALES. Both METRIC and Feet and Inches TIMES: am/pm Sunrise/Sunset Moon Phases Moon Rise/Set DIARY NOTES.

Overview ICAO Standards and Recommended Practices for Aerodrome Mapping Data reported to AIM

$6.60 NEW SOUTH WALES. Both METRIC and Feet and Inches TIMES: am/pm Sunrise/Sunset Moon Phases Moon Rise/Set DIARY NOTES.

The Past, Present, and Future of Nortek and Glider Measurements

Ground Deformation Monitoring at Natural Gas Production Sites using Interferometric SAR

NEW SOUTH WALES. Both METRIC and Feet and Inches TIMES: am/pm Sunrise/Sunset Moon Phases Moon Rise/Set DIARY NOTES.

Retreating Glaciers of the Himalayas: A Case Study of Gangotri Glacier Using Satellite Images

Space Based ADS-B. ICAO SAT meeting - June 2016 AIREON LLC PROPRIETARY INFORMATION

Trajectory Optimization for Safe, Clean and Quiet Flight

STATE -OF-ART OF GEODESY IN THE REPUBLIC OF MACEDONIA

Chapter 7 Snow and ice

Challenges in Complex Procedure Design Validation

The Rodman s Guide to Madison Vertical Datums

SUPPLEMENTARY INFORMATION

CRYOSPHERE ACTIVITIES IN SOUTH AMERICA. Bolivia. Summary

A high resolution glacier model with debris effects in Bhutan Himalaya. Orie SASAKI Kanae Laboratory 2018/02/08 (Thu)

Title: Multiplatform analysis of the Algerian Basin from satellite observations and high resolution glider data

PHY 133 Lab 6 - Conservation of Momentum

Potential of CO 2 retrieval from IASI

Overview. Eero Ailio European Commission

Glacial lakes as sentinels of climate change in Central Himalaya, Nepal

ANALYSIS OF THE CONTRIUBTION OF FLIGHTPLAN ROUTE SELECTION ON ENROUTE DELAYS USING RAMS

Environmental Assessment Las Vegas Area Airspace Optimization Project

Helicopter Vector IFR

Performance Analysis of Space-Based ADS-B

Community resources management implications of HKH hydrological response to climate variability

Air Navigation Bureau ICAO Headquarters, Montreal

EXPERIMENTAL ANALYSIS OF THE INTEGRATION OF MIXED SURVEILLANCE FREQUENCY INTO OCEANIC ATC OPERATIONS

Datum Issues in the Red River of the North Basin ----

Cal/Val Activities at the CIGSN Uardry Field Site, NSW, Australia in Support of the EO-1 Mission

Active Geodetic Network of Serbia

H-II TRANSFER VEHICLE TRAJECTORY PLANNING AND FLIGHT OPERATION RESULTS

Flight inspection and validation

ADVISORY CIRCULAR AC-AD-005

Presented by Esteban Toha G PC-IDEA vice president NSDI-Chile

Sarajevo, Bosnia and Herzegovina, February 25-27, 2009 BALGEOS

HEATHROW COMMUNITY NOISE FORUM

Historical background

TANZANIA CIVIL AVIATION AUTHORITY AIR NAVIGATION SERVICES INSPECTORATE. Title: CONSTRUCTION OF VISUAL AND INSTRUMENT FLIGHT PROCEDURES

Observations of glacier dynamics with PALSAR DATA

New measurements techniques

Introduction to the Data Catalogue

COSMO-Coast. L Aquila. La Sapienza. Tor Vergata. Dipartimento di Architettura ed Urbanistica. Dipartimento di Informatica, Sistemi e Produzione,

Magnetospheric MultiScale Mission. SpaceWire Implementation

Single Line Tethered Glider

AN-Conf/12-WP/162 TWELFTH THE CONFERENCE. The attached report

Advisory Circular AC61-3 Revision 11 SUPERSEDED Define and identify, on a diagram of the earth, and explain the meaning of the following:

L 342/20 Official Journal of the European Union

Aeronautics Math. Douglas Anderson Arellanes Junior High School Santa Maria-Bonita School District

Glossary. basic empty weight (GAMA). Standard empty weight plus optional equipment.

Formulation of Lagrangian stochastic models for geophysical turbulent flows

Rolling with Roller Coasters

Modeling Visitor Movement in Theme Parks

Competence Requirements for eronautical eteorological ersonnel

Motivations, Opportunities and Challenges of Additive Manufacturing for Space Application

ABSTRACT TIES TO CURRICULUM TIME REQUIREMENT

Airspace Complexity Measurement: An Air Traffic Control Simulation Analysis

ICAO CORSIA CO 2 Estimation and Reporting Tool (CERT) Design, Development and Validation

AERONAUTICAL SURVEYS & INSTRUMENT FLIGHT PROCEDURES

A SEGMENTED ARCHITECTURE APPROACH TO PROVIDE A CONTINUOUS, LONG-TERM, ADAPTIVE AND COST- EFFECTIVE GLACIERS MONITORING SYSTEM

April 16, Erik Larson

Wake Turbulence Research Modeling

Performance. Aircraft System

ICAO Global Provisions and Regional Strategy for the Introduction of GNSS Services in Africa-Indian Ocean (AFI) Region

ENR 1.7 ALTIMETER SETTING PROCEDURES

PERFORMANCE MEASURE INFORMATION SHEET #16

Integrated Flight Instrument Systems

Wake Encounter In-Situ Flight Tests in Cruise - Wake Characterization

Australian New Zealand Geodetic VLBI Network Project

Muography on Puy de Dôme. C Cârloganu LPC Clermont Ferrand IN2P3/CNRS

Analysis of Air Transportation Systems. Airport Capacity

Roadmapping Breakout Session Overview

Comparison Study between Vault Seismometers and a New Posthole Seismometer

Airspace Encounter Models for Conventional and Unconventional Aircraft

A GEOGRAPHIC ANALYSIS OF OPTIMAL SIGNAGE LOCATION SELECTION IN SCENIC AREA

Tidewater Glaciers: McCarthy 2018 Notes

Planned Orbital Flight Test of a 6m HIAD

GFAC CHAIRMAN'S REPORT

RNP AR APCH Approvals: An Operator s Perspective

GREEK ARGO PROGRAMME PRESENT STATUS AND FUTURE PLANS. G. Korres and D. Kassis HCMR March, 2015

Analyzing Risk at the FAA Flight Systems Laboratory

FORT LAUDERDALE-HOLLYWOOD INTERNATIONAL AIRPORT ENVIRONMENTAL IMPACT STATEMENT DRAFT

PROGRESS ON THE DESIGN STUDIES OF THE 300AMeV SUPERCONDUCTING CYCLOTRON

Time-Space Analysis Airport Runway Capacity. Dr. Antonio A. Trani. Fall 2017

AIS-AIMSG/12-SN/3 - Appendix A. New Annex 15. (Consolidated draft, 14 OCT 2015)

RUAT Junior Glider Design Competition Version 1.5

Warming planet, melting glaciers

Using LiDAR to study alpine watersheds. Chris Hopkinson, Mike Demuth, Laura Chasmer, Scott Munro, Masaki Hayashi, Karen Miller, Derek Peddle

PBN Airspace Design Workshop. Area Navigation. Asia and Pacific Regional Sub-Office Beijing, China. 5 May 2016 Page 1 APAC RSO BEIJING

Chapter 9 Validation Experiments

Clustering radar tracks to evaluate efficiency indicators Roland Winkler Annette Temme, Christoph Bösel, Rudolf Kruse

Policy and Procedures Documents for the State Plane Coordinate System of 2022

DEMETER satellite disposal, CNES give an example of French Space Act compliance. Florence DUCHEVET & Henri DARNES - CNES

Time Benefits of Free-Flight for a Commercial Aircraft

Transcription:

Height System Unificationand GOCE Reiner Rummel, Michael Sideris, Phil Woodworth 14th Canadian Geoid Workshop, Banff/Alberta, June 5, 2012

GOCE basic facts Gravity andsteady stateoceancirculationexplorer launched on March 17, 2009 (now 2½ years in orbit) first mission of ESA s Living Planet programme (followed by SMOS and CRYOSAT) mission goals: gravity with 1 ppm (1 mgal) accuracy geoid with 1 to 2 cm accuracy spatial resolution 100km (equivalent to degree/order = 200 in spherical harmonics) orbit characteristics inclination 96.5 (sun synchronous) polar data gaps circular altitude 265km! mission duration: medium 2013 18 monthsdata processed

GOCE gravity gradiometry measurement principle: acceleration differences GOCE: firstgravitationalgradiometer

GOCE gravity gradiometry 2 2 Vxx Vxy Vxz ω y ωz ωω x y ωxωz 0 ωz ωy 2 2 Vyx Vyy Vyz + ωω y x ωz ωx ωω y z + ωz 0 ωx 2 2 Vzx Vzy V zz ωω z x ωzωy ωx ω y ωy ωx 0 Y GRF Y A A Y 2 6 O 6 X X O2 6 2 Z 6 6 Z 2 2 A Y X X A 4 O4 Y 1 O1 X 1 Z 1 1 O 4 GRF GRF Z 4 4 A Y A Y 5 3 O O3 X 5 X 5 3 Z 5 5 Z 3 3 Z GRF Basic facts: 1.Measurementstaken in a rotatingframe 2. Eachaccelerometer withtwo ultra precise andone robust axis 3. Noise is white onlyinside themeasurement band (MB) from 5mHz to 0.1Hz (belowincreaseas 1/f) skew symmetric

GOCEsensorsystem ion thrusters xenon tank nitrogen tank power supply star sensor gravitational gradiometer GPS receiver source: ESA ion thruster control unit magneto torquers control unit an orbiting gravitational laboratory high performance of all sensors very different from typical remote sensing satellites

GOCE gravitymodels Global GOCE Gravity Field Models Model Data D/O Characteristics DIR1 2 Months 240 Direct Approach: Prior model (combined) plus GOCE orbits & gradiometry DIR2 6 Months 240 Direct Approach: Prior model (GRACE-only) plus GOCE orbits & gradiometry DIR3 1 Year 240 Direct Approach: Prior model (GRACE-only normals) plus GOCE gradiometry TIM1 2 Months 224 Time-wise Approach: Pure GOCE (kin. orbits & gradiometry) TIM2 6 Months 250 Time-wise Approach: Pure GOCE (kin. orbits & gradiometry) TIM3 1 Year 250 Time-wise Approach: Pure GOCE (kin. orbits & gradiometry) SPW1 2 Months 210 Space-wise Approach: GRACE low d/o plus GOCE gradiometry SPW2 6 Months 240 Space-wise Approach: Pure GOCE (kin. Orbits &gradiometry) GOCO01s 2 Months 224 Time wiseand ITG Grace2010s (d/o 180) GOCO02s 8 Months 250 Time wiseand ITG Grace2010s (d/o 180) + CHAMP+SLR

GOCE reprocessing Combinedprocessingof all threestartrackers Optimizedattitudedetermination Optimized angular rate reconstruction Interpolation ofcalibrationmatrices Brockmann, Schuh, Krasbutter, 2012 Technical Note 11.05.2012

GOCE reprocessing GPS leveling vs. GOCE & EGM2008 Canada USA Th Gruber, 2012

Status of GOCE Launch in March 2009; sciencedatasince November 2009 GOCE combines (fouraccurate) gradiometercomponentsv xx, V yy, V zz andv xz andorbittrackingby GPS Itsstrengthareprimarilytheshorterspatialscales, say> d/o 80 Approximatelyonefullyearofdataprocessedby HPF Currently level 1b re processing (combinationof 3 STRs, improved angular rate reconstruction, interpolationofcalibrationmatrices) mainimprovementsexpectedatlongspatialscales Commissionerrordecreaseswiththesqrtoffullorbitcycles (each 31 days)

GOCE and GRACE 10-6 SLR GRACE GOCE Mean Signal per Degree / Degree Error Median 10-7 10-8 10-9 10-10 10-11 10-12 Mean Signal QL GOCE Model Mean Signal Kaula Rule ErrorMedianQLGOCEModel Error Median EIGEN-5S Error Median EIGEN-5C temporal variations GRACE GOCE 50 100 150 200 Degree 400km 200km 100km degreevariances (median) ofsignalandnoise

GOCE and GRACE Yi W, 2011 Contribution anylysis of a GOCE GRACE combination

GOCE versus EGM2008 3.0 2.5 36.0 33.0 3.5 23.0 11.0 in cm RMS geoiddifferencesbetween EGM2008 and GOCE release 3 wellsurveyedregions (black), problematicregions (red) andantarctica (green)

GOCE versus EGM2008 Yi & Rummel, 2012 Geoid differences GOGRA vs. EGM08

GOCE versus EGM2008 EGM2008 5 arc minute areameangravityanomalies datasources Pavlis et al., 2012)

GOCE overview GOCE special issue of Journal of Geodesy Volume 85, no.11, 2011

GOCE scienceandapplication point of departure solid earth ocean ice geodesy sea level gravity anomalies seismic tomograpy geoid gravity anomalies geoid + + + + ocean altimetry ice topography positioning (GPS) tide gauges altimetry topography deformations laboratory mean ocean circulation bedrock topography levelled heights post glacial rebound unified height system mean ocean circulation anomalous density structure constraints on mass & heat transport mass balance of ice sheets gravity anomalies ice mass balance orbits unified height systems INS orbits Granada, 1999

GOCE andheightsystemunification ESA s Support Top Science Element (STSE) An elementofthe Earth Observation Envelope Programme 3 Theme 1: Height System Unificationwith GOCE (STSE HSU) Team: IAPG, Technical University Munich (coordination) University of Calgary BKG, Frankfurt/Main NOC Liverpool andconsultants

GOCE andheightsystemunification The nineitemsofthisstudy: 1. State-of-the-art in heightsystemsandtheirunification 2. Quantificationofknowndifferences 3. Review, evaluationandimprovementofmethodology 4. Attemptof global height (andtidegauge) unification 5. Selectionoftwotestregions effectof GOCE 6. Effectofunification on localgravityandtopographicheights 7. Geophysicalinterpretation: dynamicoceantopography, currents, 8. Involvementoflocal/ national authorities 9. Roadmap forfutureworkusing GOCE: worldheightsystem andverticaldatum

GOCE andheightsystemunification Perspective With GOCE gravity models a significant improvement of the global geoid can be reached. Models based on 1 year of data reach a global geoid error of 4.6 cm at 100 km resolution. With a successful extended mission of GOCE this can be further improved to better than 2.9 cm after 2012. 10.0 6.1 4.6 2.9 *) from: R. Pail, IAPG

Structureandstatusof STSE GOCE HSU WP200: Preliminary Analysis Existing methods (210) Review (240-270) VC propagation (220) GBVP approach (230) Optimal combination (280) Regional studies: North America North Atlantic Europe/Germany WP500: Impact Assessment Quality analysis of global simulation (540) GOCE regional impact assessment (510-530, 550) WP100: Requirements Consolidation WP400: Development & Validation Global unification simulator and error propagation (410) Regional unification and error assessment (420-440) WP300: Data Collection & Promo. Web page (310, 320) Data collection (320-340) Promotion (350) WP600: Scientific Roadmap Geodetic application (620) Roadmap regional unification and application (610, 630, 640) Roadmap global unification GGOS, IAG, WHS (650)

GOCE andheightsystemunification Vertical Reference Frame Definition The realization of a system for elevations that supports physical and geometric heights globally with ppb relative accuracy Vertical Datum A level, zero-height surface with a conventional value W o A W o value does not imply knowledge of the level surface itself Realization and Unification Data: GNSS/SLR, geodetic & ocean leveling, TGs, altimetry, gravity, GGMs Zero-tide system (BVP solution requirement) Convert C to H or H*, or vice versa Select/determine global W o value Determine local W oj values and connect W oj to W o C P = W o W P = dw = gdh P P o P P o

GOCE andheightsystemunification Vertical Reference Frame W o can be obtained from, e.g., ellipsoidal parameters (W o = U o ), or computed/assigned to a tide gauge or from a GGM and/or altimetry and/or MSL fit or from the solution of a (generalized) geodetic BVP W P can be obtained either from the BVP solution for T P W P = U P + T P or from levelling plus gravity (given W o ) C P = W o W P = gδn or from GNSS/SLRand geodetic/ocean levelling T P = gn P =g(h P H P ) Consistent use of standards, theory and data is essential

GOCE andheightsystemunification Solution of the height datum problem North America North Atlantic Europe

GOCE andheightsystemunification The GBVP approach Global offset No δ ( GM ) ΔWo ( h H j ) N = + Rγ γ C γ jo Geoid from GPS/levelling Geoid from solution of GBVP Regional offset Njo Gravimetric geoid with biased gravity anomalies R 2 N = S( ψ ) Δg j + C jo dω, 4πγ Ω R g Δg j = g H j γ h

GOCE andheightsystemunification GOCEgeoid: Limited resolution Omission error 30 cm Commission error 1 2 cm The GBVP approach N GOCE = GM Rγ L max l P (cosθ )( ΔC cos mλ +ΔS lm l= 2 m= 0 lm lm sin mλ) GOCE N = N + N res N res = R res res S ( ψ ) Δg j dω + 4πγ Ω 1 S 2πγ Ω res ( ψ ) C jo dω Biased residual geoid Indirect bias term

GOCE andheightsystemunification functionalpart adjustmentmodel stochasticpart land topography 8000m A O c C B H c h(c) H b h(b) N(C) N(B) O b mean dynamic ocean topography (MDT) ±1 to 2m O a h(a) H a N(A) geoid reference ellipsoid

GOCE andheightsystemunification Variance covariance propagation for GOCE Comparable precision of h, H, N, or ζ and proper stochastic models GOCEVCM, d/o 250 for the first orders m=0,1,2,3 HSU simulator for error analysis and impact assessment GOCO2s up to d/o 200: Geoid height error Full Error VCM m block approximation

GOCE andheightsystemunification Geometric and Gravimetric Coordinate System consistency The N1 term in the geoid height should be added if GOCE is not geo localized in a geocentric reference frame Center of mass in a geocentric reference system

GOCE andheightsystemunification Evaluation of the Indirect Bias Term All offsets are computed with respect to the global level surface defined by 2 2 W o = 62636856.00 m / s

GOCE andheightsystemunification Evaluation of the Indirect Bias Term Stokes kernel

GOCE andheightsystemunification Evaluation of the Indirect Bias Term Truncated Stokes kernel: Lmax= 150

GOCE andheightsystemunification Evaluation of the Indirect Bias Term

GOCE andheightsystemunification Effect of the Omission Error Mean differences between the regional GPS/levelling geoid heights and GOCEgeoid heights computed by means of TIM_R3, d/o=200

GOCE andheightsystemunification Effect of the Omission Error North America: Datum offsets computed with EGM2008 truncated to different d/o (of the available satellite only and combined global gravity models)

GOCE andheightsystemunification Effect of the Omission Error A simulation study: minimum size of the averaging area with GPS/levelling stations for which the mean omission error is few centimeters neglect res the N term.

GOCE andheightsystemunification Effect of the Omission Error Average Area Point (1) The mean omission error is at a cm level (2) In all cases, the difference between area and point averages is below 2cm (exception: Switzerland) (3) Larger differences between observed and simulated mean omission error might indicate systematic effects

GOCE andheightsystemunification Height Unification Using Ocean Information NOCL Objectives: (1)Collect tide gauge, GPS, altimeter, ocean model and geoid information so as to compare MSL differences (adjusted by the models) to geoid differences over a given epoch at and near the coast (in the case of tide gauges and altimetry respectively) (2)Thereby both validate the new geoid models, and obtain confidence in the use of ocean models to relate MSL (and so datums) in one country to that in another. PSMSLRLR Stations (> 40 Years of Data)

MSL above National Datums North Atlantic Nova Scotia

MSL above National Datums North Pacific USA MSL approximately 1 metre above datum on the Pacific coast

MSL minus Geoid (GOCO03Sp) N America Atlantic Outlier Reedy Point

MSL minus Geoid (Extended Model) N America Atlantic Outliers Reedy Point and Portland (maybe Fernandina Beach)

GOCE andheightsystemunification Project Website http://www.goceplushsu.eu/

GOCE andheightsystemunification Outlook (1) Development of global height system unification simulator and error propagation (2) Implementation of the least squares adjustment model (3) Regional unification of height systems in Europe and North America (4) Connecting Europe and North America using (i) the GBVP approach and (ii) using ocean information (5) Quality analysis and interpretation of height unification results with the GBVP approach (6) Assessment of improvement in height unification with and without the GOCEgeoid (7) Assessment of improvement in consistency between geodetic and oceanographic insights into spatial variation in sea level on regional and basin scales. (8) Developing a roadmap for regional and global height system unification