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GPS Radio Occultation with CHAMP, GRACE-A, Terrasar-X, and COSMIC: Brief Review of Results from GFZ J
GPS radio occultation with CHAMP, GRACE-A, TerraSAR-X, and COSMIC: Brief review of results from GFZ J. Wickert, G. Beyerle, C. Falck, S. Heise, R. König, G. Michalak, D. Pingel*, M. Rothacher, T. Schmidt, and C. Viehweg GeoForschungsZentrum Potsdam, * Deutscher Wetterdienst Overview Current GPS occultation missions During the last decade ground and space based GNSS techniques for atmospheric/ionospheric remote sensing were established. The currently increasing number of receiver platforms (e.g., extension of regional/global ground networks and additional LEO satellites) together with future additional transmitters (GALILEO, reactivated GLONASS, new signal structures for GPS) will extend the potential of these innovative sounding techniques during the next years. Here, we focus to GPS radio CHAMP GRACE TerraSAR-X occultation and present selected examples of recent GFZ results. The activities include orbit and atmospheric /ionospheric occultation data processing for several satellite mission (CHAMP,GRACE-A, SAC-C, and COSMIC), but also various applications. Data sets from CHAMP, GRACE and COSMIC MetOp COSMIC SAC-C Current GPS radio occultation missions: CHAMP (launch July 15, 2000), GRACE (March 17, 2002), TerraSAR-X (June 15, 2007), MetOp (October 18, 2006), COSMIC (April 15, 2006) and SAC-C(November 21, 2000). Number of daily available vertical atmospheric profiles, derived from CHAMP (left), GRACE (middle), and COSMIC (right, UCAR processing) measurements (note the different scale). COSMIC provides significantly more data compared to CHAMP and GRACE-A. The long-term set from CHAMP is unique (300 km orbit altitude expected in Dec. 2008). Validation of CHAMP with MOZAIC aircraft data Near-real time data from CHAMP and GRACE-A (a) (b) (c) GFZ provides near-real time occultation data (bending angle and refractivity profiles) from CHAMP and GRACE-A using it’s operational ground infrastructure including 2 receiving antennas at Ny Ålesund. -
A Survey and Assessment of the Capabilities of Cubesats for Earth Observation
Acta Astronautica 74 (2012) 50–68 Contents lists available at SciVerse ScienceDirect Acta Astronautica journal homepage: www.elsevier.com/locate/actaastro Review A survey and assessment of the capabilities of Cubesats for Earth observation Daniel Selva a,n, David Krejci b a Massachusetts Institute of Technology, Cambridge, MA 02139, USA b Vienna University of Technology, Vienna 1040, Austria article info abstract Article history: In less than a decade, Cubesats have evolved from purely educational tools to a standard Received 2 December 2011 platform for technology demonstration and scientific instrumentation. The use of COTS Accepted 9 December 2011 (Commercial-Off-The-Shelf) components and the ongoing miniaturization of several technologies have already led to scattered instances of missions with promising Keywords: scientific value. Furthermore, advantages in terms of development cost and develop- Cubesats ment time with respect to larger satellites, as well as the possibility of launching several Earth observation satellites dozens of Cubesats with a single rocket launch, have brought forth the potential for University satellites radically new mission architectures consisting of very large constellations or clusters of Systems engineering Cubesats. These architectures promise to combine the temporal resolution of GEO Remote sensing missions with the spatial resolution of LEO missions, thus breaking a traditional trade- Nanosatellites Picosatellites off in Earth observation mission design. This paper assesses the current capabilities of Cubesats with respect to potential employment in Earth observation missions. A thorough review of Cubesat bus technology capabilities is performed, identifying potential limitations and their implications on 17 different Earth observation payload technologies. These results are matched to an exhaustive review of scientific require- ments in the field of Earth observation, assessing the possibilities of Cubesats to cope with the requirements set for each one of 21 measurement categories. -
The Impact of Satellite Data in the Joint Center for Satellite
The Impact of Satellite Data in the Joint Center for Satellite Data Assimilation John Le Marshall (JCSDA) Director, JCSDA 2004-2007 Lars-Peter Rishojgaard 2007- … Overview • Background • The Challenge • The JCSDA • The Satellite Program • Recent Advances • Impact of Satellite Data • Plans/Future Prospects • Summary CDAS/Reanl vs GFS NH/SH 500Hpa day 5 Anomaly Correlation (20-80 N/S) 90 NH GFS 85 SH GFS NH CDAS/Reanl 80 SH CDAS/Reanl 75 70 65 60 Anomaly Correlation Anomaly Correlation 55 50 45 40 1960 1970 1980 1990 2000 YEAR Data Assimilation Impacts in the NCEP GDAS N. Hemisphere 500 mb AC Z 20N - 80N Waves 1-20 15 Jan - 15 Feb '03 1 0.9 0.8 0.7 0.6 control 0.5 no amsu 0.4 no conv 0.3 Anomaly Correlation 0.2 0.1 0 1234567891011121314151617 Forecast [days] AMSU and “All Conventional” data provide nearly the same amount of improvement to the Northern Hemisphere. Impact of Removing Selected Satellite Data on Hurricane Track Forecasts in the East Pacific Basin 140 120 100 Control No AMSU 80 No HIRS 60 No GEO Wind 40 No QSC 20 Average Track ErrorsAverage [NM] 0 12 24 36 48 Forecst Time [hours] Anomaly correlation for days 0 to 7 for 500 hPa geopotential height in the zonal band 20°-80° for January/February. The red arrow indicate use of satellite data in the forecast model has doubled the length of a useful forecast. The Challenge Satellite Systems/Global Measurements GRACE Aqua Cloudsat CALIPSO TRMM SSMIS GIFTS TOPEX NPP Landsat MSG Meteor/ SAGE GOES-R COSMIC/GPS NOAA/ POES NPOESS SeaWiFS Terra Jason Aura ICESat SORCE WindSAT 5-Order Magnitude -
Combination of Multi-Satellite Altimetry Data with CHAMP and GRACE Egms for Geoid and Sea Surface Topography Determination
Combination of multi-satellite altimetry data with CHAMP and GRACE EGMs for geoid and sea surface topography determination G.S. Vergos , V.N. Grigoriadis, I.N. Tziavos Department of Geodesy and Surveying, Aristotle University of Thessaloniki, University Box 440, 541 24, Thessalo- niki, Greece, Fax: +30 231 0995948, E-mail: [email protected]. M.G. Sideris Department of Geomatics Engineering, University of Calgary, Abstract. Since the launch of the first altimetric mis- repeating measurements of the sea surface. Such satel- sions a wealth of data for the sea surface has become lites are ERS1, ERS2 and ENVISAT and available and utilized for geoid and sea surface topogra- TOPEX/Poseidon (T/P) with JASON-1. JASON-1 and phy modeling. The data from the gravity field dedicated ENVISAT are the latest on orbit satellites (December satellite missions of CHAMP and GRACE provide a 2001 and March 2002, respectively) and are both set on unique opportunity for combination studies with satel- exact repeat missions (ERM). lite altimetric observations. This study focuses on the This long series of altimetric observations has been combination of data from GEOSAT, ERS1/2, widely used for studies on the determination of MSS Topex/Poseidon, JASON-1 and ENVISAT with Earth models (Andersen and Knudsen 1998; Cazenave et al. Gravity Models (EGMs) generated from CHAMP and 1996), global and regional geoid models (Andritsanos et GRACE data to study the mean sea surface al. 2001; Lemoine et al. 1998; Vergos et al. 2005) as (MSS)/marine geoid in the Mediterranean Sea. Various well as on the recovery of gravity anomalies from al- combination methods, i.e., weighted least squares and timetric measurements (Andersen and Knudsen 1998; least squares collocation are investigated and conclu- Hwang et al. -
Landsat 9 Micrometeoroid and Orbital Debris Mission Success Approach
First Int'l. Orbital Debris Conf. 2019 (LPI Contrib. No. 2109) 6058.pdf Landsat 9 Micrometeoroid and Orbital Debris Mission Success Approach Michael S. Pryzby(1), Scott M. Hull(2), Angela M. Russo(2), Glenn T. Iona(2), Daniel Helfrich(2), and Evan H. Webb(2) (1) ATA Aerospace, 7474 Greenway Center Dr, Suite 500, Greenbelt, MD 20770, USA (2) NASA Goddard Space Flight Center, 8800 Greenbelt Rd, Greenbelt, MD 20771, USA ABSTRACT Landsat 9* (L9) is the successor mission to Landsat 8 (L8) previously known as Landsat Data Continuity Mission (LDCM). Both missions are large unmanned remote sensing satellites operating in sun- synchronous polar orbits. As opposed to L8/LDCM, systems engineers for L9 incorporated Micrometeoroid/Orbital Debris (MMOD) protection for small object collisions as part of the L9’s mission success criteria. In other words, the NASA Process for Limiting Orbital Debris (NASA-STD-8719.14A) only calls for analyses of the protection of disposal-critical hardware, but L9 opted to also assess and provide small particle penetration protections for all observatory components including instruments that are not part of the spacecraft components needed for controlled reentry. Systems engineers at Goddard developed a design process to protect against MMOD during the life of Low Earth Orbit (LEO) observatories, and in particular the Landsat 9 Mission. Simply stated, this design process enhanced the effectiveness of existing Multi-Layer Insulation (MLI) to provide the needed protection. The end goal of the design process was to establish a necessary blanket areal density for a given electronics box or instrument wall thickness and a separation between the outer MLI blanket and the structure underneath. -
Gravity Field Analysis from the Satellite Missions CHAMP and GOCE
Institut fÄurAstronomische und Physikalische GeodÄasie Gravity Field Analysis from the Satellite Missions CHAMP and GOCE Martin K. Wermuth VollstÄandigerAbdruck der von der FakultÄatfÄurBauingenieur- und Vermessungswesen der Technischen UniversitÄatMÄunchen zur Erlangung des akademischen Grades eines Doktor-Ingenieurs (Dr.-Ing.) genehmigten Dissertation. Vorsitzender: Univ.-Prof. Dr.-Ing. U. Stilla PrÄuferder Dissertation: 1. Univ.-Prof. Dr.-Ing., Dr. h.c. R. Rummel 2. Univ.-Prof. Dr.-Ing. N. Sneeuw, UniversitÄatStuttgart Die Dissertation wurde am 04.03.2008 bei der Technischen UniversitÄatMÄunchen eingereicht und durch die FakultÄatfÄurBauingenieur- und Vermessungswesen am 04.07.2008 angenommen. Zusammenfassung In dieser Arbeit ist die Bestimmung von globalen Schwerefeldmodellen aus Beobachtungen der Satelliten- missionen CHAMP und GOCE beschrieben. Im Fall von CHAMP wird die sogenannte Energieerhaltungs- Methode auf GPS Beobachtungen des tief fliegenden CHAMP Satelliten angewandt. Im Fall von GOCE ist Gradiometrie die wichtigste BeobachtungsgrÄo¼e.Die Erfahrung die bei der Verarbeitung von Echt- daten der CHAMP Mission gewonnen wurde, fließt in die Entwicklung einer operationellen Quick-look Software fÄurdie GOCE Mission ein. Die Aufgabe globaler Schwerefeldbestimmung ist es, aus Beobach- tungen entlang einer Satellitenbahn ein Model des Gravitationsfeldes der Erde abzuleiten, das auf der Erdoberfl¨ache in sphÄarisch-harmonischen Koe±zienten beschrieben wird. Die theoretischen Grundla- gen, die nÄotigsind um die Beobachtungen mit dem Schwerefeld in Bezug zu setzen und ein globales Schwerefeld aus Satellitenbeobachtungen zu berechnen sind werden ausfÄuhrlich erklÄart. Die CHAMP Mission wurde im Jahr 2000 gestartet. Sie ist die erste Schwerefeldmission mit einem GPS EmpfÄangeran Bord. Die HauptbeobachtungsgrÄo¼ensind die GPS Bahn-Beobachtungen zu CHAMP, das sogenannte "satellite-to-satellite tracking" (SST). Ein Schwerefeldmodell wird mit der Energieerhaltungs- Methode unter Verwendung von kinematischen Bahnen berechnet. -
A Prototype WRF-Based Ensemble Data Assimilation System for Dynamically Downscaling Satellite Precipitation Observations
118 JOURNAL OF HYDROMETEOROLOGY VOLUME 12 A Prototype WRF-Based Ensemble Data Assimilation System for Dynamically Downscaling Satellite Precipitation Observations DUSANKA ZUPANSKI* CIRA/Colorado State University, Fort Collins, Colorado SARA Q. ZHANG NASA Goddard Space Flight Center, Greenbelt, Maryland MILIJA ZUPANSKI CIRA/Colorado State University, Fort Collins, Colorado ARTHUR Y. HOU NASA Goddard Space Flight Center, Greenbelt, Maryland SAMSON H. CHEUNG University of California, Davis, Davis, California (Manuscript received 12 January 2010, in final form 23 August 2010) ABSTRACT In the near future, the Global Precipitation Measurement (GPM) mission will provide precipitation observations with un- precedented accuracy and spatial/temporal coverage of the globe. For hydrological applications, the satellite observations need to be downscaled to the required finer-resolution precipitation fields. This paper explores a dynamic downscaling method using ensemble data assimilation techniques and cloud-resolving models. A prototype ensemble data assimilation system using the Weather Research and Forecasting Model (WRF) has been developed. A high-resolution regional WRF with multiple nesting grids is used to provide the first-guess and ensemble forecasts. An ensemble assimilation algorithm based on the maximum likelihood ensemble filter (MLEF) is used to perform the analysis. The forward observation operators from NOAA–NCEP’s gridpoint statistical interpolation (GSI) are incorporated for using NOAA–NCEP operational datastream, including conven- tional data and clear-sky satellite observations. Precipitation observation operators are developed with a combination of the cloud-resolving physics from NASA Goddard cumulus ensemble (GCE) model and the radiance transfer schemes from NASA Satellite Data Simulation Unit (SDSU). The prototype of the system is used as a test bed to optimally combine observations and model information to produce a dynamically downscaled precipitation analysis. -
Étude De Faisabilité Télédétection De L'écoulement De Surface Provenant D'amas Au Champ Et Enclos D'hivernage
Étude de faisabilité Télédétection de l’écoulement de surface provenant d’amas au champ et enclos d’hivernage Présentée au : Ministère Développement durable, Environnement et Parcs Direction des politiques en milieu terrestre Édifice Marie-Guyart, 9e étage, boîte 71 675, boulevard René-Lévesque Est, Québec (Québec), G1R 5V7 Par Karem Chokmani, professeur Lisa-Marie Pâquet, assistante de recherche Yves Gauthier, agent de recherche Institut national de la recherche scientifique – Eau, Terre & Environnement 490 rue de la Couronne, Québec (Québec), G1K 9A9 Tél. : (418) 654-2570 Téléc. : (418) 654-2600 Courriel : [email protected] Rapport de recherche N° R-979 Avril 2008 ISBN : 978-2-89146- 568-7 ii AVANT PROPOS Dans le cadre des efforts du ministère du développement durable, de l’environnement et des parcs (MDDEP) pour valider et bonifier les connaissances sur la conception des amas de fumier au champ, l’équipe de recherche de l’INRS-ETE, sous la direction du professeur Karem Chokmani, a été mandaté par le ministère pour réaliser une étude de faisabilité pour la télédétection de l’écoulement de surface provenant d’amas au champ et d’enclos d’hivernage. Dans le présent rapport de recherche, après une section d’introduction consacrée à la problématique et aux objectifs, une synthèse de la revue de littérature et un exposé de la méthodologie de travail y sont présentés. Les résultats sont par la suite décrits et discutés pour finir avec les conclusions ainsi qu’une série de recommandations concernant la faisabilité de l’approche et la démarche à suivre pour son éventuelle application opérationnelle. -
Bob Cabana, Director Kennedy Space Center National Aeronautics and Space Administration
Bob Cabana, Director Kennedy Space Center National Aeronautics and Space Administration Premier Multi-User Spaceport KSC Programs and Projects Commercial Crew Program Launch Services Program Exploration Ground Systems Gateway — A spaceport for human and Exploration Research & Technology robotic exploration to the Moon and beyond Programs 2019 KSC Key Milestones o March 2 SpaceX Demo-1 LC 39A o June 27 Mobile Launcher rolls testing to SLC 39B o July 2 Orion Launch Abort System Test SLC-46 o October 10 ICON Mission CCAFS Remaining Milestones Planned in 2019 Boeing Pad Abort Test – Target date 11/4/19 Boeing Orbital Flight Test – Target date mid December SpaceX In-Flight Abort Test – Target date early December Gateway Logistics Contract Award 2020 KSC Key Milestones Orion Mass Simulator on dock KSC - 1/24/20 SpaceX Demo-2 Boeing Crewed Flight Test Solar Orbiter – 2/5/20 SLS Boosters arrive and processing begins - 3/18/20 Orion turnover to EGS - 5/16/20 MARS 2020 -7/17/20 Sentinel 6A - 11/15/20 Landsat-9 – 12/15/20 7 National Aeronautics and Space Administration SpaceX Demo-1 March 2, 2019 Boeing Hotfire & Parachute Tests May 22, 2019 National Aeronautics and Space Administration High Performance Spaceflight Computing Precision Solar Landing Electric Space Technology for Propulsion 2024 and Beyond Surface Cryofluid Lunar Dust Excavation/Construction Management Mitigation In Situ Resource Extreme Environments Utilization Extreme Access Lunar Surface Power Lunar Surface Innovation Initiative NASA Internal Use Only Do Not Distribute 18 EGS Striving Toward Launch of Artemis I SLS Block 1 National Aeronautics and Space Administration Orion Liquid oxygen Artemis I Intertank Core Stage 322 feet 322 Booster Mobile Launcher 130 feet 130 Rocket Crew Access Arm 274 feet 274 feet 380 Engine NASA Internal Use Only Do Not Distribute Vehicle Assembly Building 380 feet • 10.5 million lbs. -
Spectral Response Characterization of the Landsat 9 Operational Land Imager 2 Using the Goddard Laser for Absolute Measurement of Radiance (GLAMR)
Spectral Response Characterization of the Landsat 9 Operational Land Imager 2 using the Goddard Laser for Absolute Measurement of Radiance (GLAMR) Brian Markham, Julia Barsi, Joel McCorkel, Brendan McAndrew, Jeffrey Pedelty, + GLAMR and Ball I & T and Systems teams NASA Goddard Space Flight Center Mission Objectives Mission Parameters • Provide continuity in multi-decadal Landsat land surface observations to • Single Satellite, Mission Category 1, Risk Class B study, predict, and understand the consequences of land surface dynamics • 5-year design life after on-orbit checkout • Core Component of Sustainable Land Imaging program • At least 10 years of consumables • Sun-synchronous orbit, 705 km at equator, 98°inclination • 16-day global land revisit • Partnership: NASA & USGS Mission Team • NASA: Flight segment & checkout • NASA Goddard Space Flight Center (GSFC) • USGS: Ground system and operations • USGS Earth Resources Observation & Science (EROS) Center • Category 3 Launch Vehicle • NASA Kennedy Space Center (KSC) • Launch: Management Agreement - December 2020 Agency Baseline Commitment – November 2021 Instruments • Operational Land Imager 2 (OLI-2; Ball Aerospace) • Reflective-band push-broom imager (15-30m res) • 9 spectral bands at 15 - 30m resolution • Retrieves data on surface properties, land cover, and vegetation condition • Thermal Infrared Sensor 2 (TIRS-2; NASA GSFC) • Thermal infrared (TIR) push-broom imager • 2 TIR bands at 100m resolution • Retrieves surface temperature, supporting agricultural and climate applications, including monitoring evapotranspiration Spacecraft (S/C) & Observatory Integration & Test (I&T) • Northrop Grumman Innovation Systems (NGIS), formerly Orbital ATK (OA) Launch Services • United Launch Alliance (ULA) Atlas V 401 Increase in pivot irrigation in Saudi Arabia from 1987 to 2012 as recorded by Landsat. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 1 January–April 2019 CONTENTS SPACE POLICY AND PROGRAMMES .................................................................................... 1 Focus .................................................................................................................... 1 Europe ................................................................................................................... 4 11TH European Space Policy Conference ......................................................................... 4 EU programmatic roadmap: towards a comprehensive Regulation of the European Space Programme 4 EDA GOVSATCOM GSC demo project ............................................................................. 5 Programme Advancements: Copernicus, Galileo, ExoMars ................................................... 5 European Space Agency: partnerships continue to flourish................................................... 6 Renewed support for European space SMEs and training ..................................................... 7 UK Space Agency leverages COMPASS project for international cooperation .............................. 7 France multiplies international cooperation .................................................................... 7 Italy’s PRISMA pride ................................................................................................ 8 Establishment of the Portuguese Space Agency: Data is King ................................................ 8 Belgium and Luxembourg -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 2 May–June 2019 CONTENTS FOCUS ..................................................................................................................... 1 European industrial leadership at stake ............................................................................ 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 9th EU-ESA Space Council .......................................................................................... 2 Europe’s Martian ambitions take shape ......................................................................... 2 ESA’s advancements on Planetary Defence Systems ........................................................... 2 ESA prepares for rescuing Humans on Moon .................................................................... 3 ESA’s private partnerships ......................................................................................... 3 ESA’s international cooperation with Japan .................................................................... 3 New EU Parliament, new EU European Space Policy? ......................................................... 3 France reflects on its competitiveness and defence posture in space ...................................... 3 Germany joins consortium to support a European reusable rocket.........................................