An Introduction to the Geostationary-NASA Earth Exchange (Geonex) Products: 1
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Earthcare and Himawari-8 Aerosol Products
EarthCARE and Himawari-8 Aerosol Products Maki Kikuchi, H. Murakami, T. Nagao, M. Yoshida, T. Nio, Riko Oki (JAXA/EORC), M. Eisinger and T. Wehr (ESA/ESTEC), EarthCARE project members and Himawari-8 group members 14th July 2016 Contact: [email protected] EarthCARE Earth Observation Research Center 2 CPR Observation Instruments on EarthCARE MSI CPRCPR Cloud Profiling Radar BBR ATLIDATLID Atmospheric Lidar ATLID Copyright ESA MSIMSI Multi-Spectral Imager European Space Agency(ESA)/National Institute of Institutions Information and Communications Technology(NICT)/ BBRBBR Broadband Radiometer Japan Aerospace Exploration Agency(JAXA) Launch 2018 using Soyuz or Zenit (by ESA) Mission Duration 3-years Mass Approx. 2200kg Sun-synchronous sub-recurrent orbit Orbit Altitude: approx. 400km Mean Local Solar Time (Descending): 14:00 Synergetic Observation by 4 sensors Repeat Cycle 25 days Orbit Period 5552.7 seconds Semi Major Axis 6771.28 km Eccentricity 0.001283 3 Inclination 97.050° 285m Synergetic Observation by 4 Sensors on Global Scale •3‐dimensional structureGlobal simultaneous of aerosol observations and cloud of including vertical motion ‐ Cloud & aerosol profiles, 3D structure, with vertical motions •Radiation flux at top of‐ Radiation atmosphere flux at Top of Atmosphere (TOA) •Aerosol –cloud –radiation‐ Aerosol interactions‐Cloud‐Radiation interaction 4 ATLID ATLID Global Observation of Cloud and Atmospheric Lidar Aerosol Vertical Profile and Optical Properties 355nm High Spectral Resolution Lidar ATLID is a High Spectral Resolution Lidar (HSRL) developed by Instrument (HSRL) European Space Agency. - Rayleigh Channel Channel - Mie Channel(Cross-polarization) Different from the traditional Mie lidar, it has the capability to - Mie Channel (Co-polarization) separate Rayleigh scattering signal (originate from Sampling Horizontal : 285m / Vertical : 103m atmospheric molecules) and Mie scattering signal (originate Observation 3°Off Nadir(TBD) from aerosol and cloud) by high spectral resolution filter. -
AFSPC-CO TERMINOLOGY Revised: 12 Jan 2019
AFSPC-CO TERMINOLOGY Revised: 12 Jan 2019 Term Description AEHF Advanced Extremely High Frequency AFB / AFS Air Force Base / Air Force Station AOC Air Operations Center AOI Area of Interest The point in the orbit of a heavenly body, specifically the moon, or of a man-made satellite Apogee at which it is farthest from the earth. Even CAP rockets experience apogee. Either of two points in an eccentric orbit, one (higher apsis) farthest from the center of Apsis attraction, the other (lower apsis) nearest to the center of attraction Argument of Perigee the angle in a satellites' orbit plane that is measured from the Ascending Node to the (ω) perigee along the satellite direction of travel CGO Company Grade Officer CLV Calculated Load Value, Crew Launch Vehicle COP Common Operating Picture DCO Defensive Cyber Operations DHS Department of Homeland Security DoD Department of Defense DOP Dilution of Precision Defense Satellite Communications Systems - wideband communications spacecraft for DSCS the USAF DSP Defense Satellite Program or Defense Support Program - "Eyes in the Sky" EHF Extremely High Frequency (30-300 GHz; 1mm-1cm) ELF Extremely Low Frequency (3-30 Hz; 100,000km-10,000km) EMS Electromagnetic Spectrum Equitorial Plane the plane passing through the equator EWR Early Warning Radar and Electromagnetic Wave Resistivity GBR Ground-Based Radar and Global Broadband Roaming GBS Global Broadcast Service GEO Geosynchronous Earth Orbit or Geostationary Orbit ( ~22,300 miles above Earth) GEODSS Ground-Based Electro-Optical Deep Space Surveillance -
Generation of GOES-16 True Color Imagery Without a Green Band
Confidential manuscript submitted to Earth and Space Science 1 Generation of GOES-16 True Color Imagery without a Green Band 2 M.K. Bah1, M. M. Gunshor1, T. J. Schmit2 3 1 Cooperative Institute for Meteorological Satellite Studies (CIMSS), 1225 West Dayton Street, 4 Madison, University of Wisconsin-Madison, Madison, Wisconsin, USA 5 2 NOAA/NESDIS Center for Satellite Applications and Research, Advanced Satellite Products 6 Branch (ASPB), Madison, Wisconsin, USA 7 8 Corresponding Author: Kaba Bah: ([email protected]) 9 Key Points: 10 • The Advanced Baseline Imager (ABI) is the latest generation Geostationary Operational 11 Environmental Satellite (GOES) imagers operated by the U.S. The ABI is improved in 12 many ways over preceding GOES imagers. 13 • There are a number of approaches to generating true color images; all approaches that use 14 the GOES-16 ABI need to first generate the visible “green” spectral band. 15 • Comparisons are shown between different methods for generating true color images from 16 the ABI observations and those from the Earth Polychromatic Imaging Camera (EPIC) on 17 Deep Space Climate Observatory (DSCOVR). 18 Confidential manuscript submitted to Earth and Space Science 19 Abstract 20 A number of approaches have been developed to generate true color images from the Advanced 21 Baseline Imager (ABI) on the Geostationary Operational Environmental Satellite (GOES)-16. 22 GOES-16 is the first of a series of four spacecraft with the ABI onboard. These approaches are 23 complicated since the ABI does not have a “green” (0.55 µm) spectral band. Despite this 24 limitation, representative true color images can be built. -
GLM Product Evaluation and Highlights of My Research at CICS
GLM Product Evaluation and Highlights of My Research at CICS Ryo Yoshida Satellite Program Division, Observation Department Japan Meteorological Agency (JMA) STAR Seminar, October 24, 2019 Overview of my research visit • “Japanese Government Short-Term Overseas Fellowship Program” sponsored by the National Personnel Authority of Japan • Period: Nov. 5, 2018 - Nov. 3, 2019 • NESDIS accepted me at CICS, based on the framework of the NESDIS-JMA high-level letter exchange on information exchange regarding GOES-R Series & Himawari-8/9 • Research topics: GLM & NOAA’s advanced efforts on satellites I deeply appreciate NESDIS’s giving me this great opportunity Japan Meteorological Agency 2 Contents 1. Overview of JMA and Himawari satellites 2. Highlights of my research at CICS 3. GLM product evaluation Japan Meteorological Agency 3 1. Overview of JMA and Himawari satellites Japan Meteorological Agency 4 What JMA is Japan’s national meteorological service, whose ultimate goals are Safety of transportation Prevention Development and mitigation and prosperity of natural of industry disasters International cooperation Japan Meteorological Agency prescribed by the Meteorological Service Act. 5 What JMA does • Weather observations • Weather forecasts and warnings • Aviation & marine weather services • Climate & global environment services • Monitoring seismic & volcanic activity & tsunamis Japan Meteorological Agency 6 JMA’s weather observation systems 16 radiosonde stations 33 wind profilers Upper air observations Geostationary satellites Observations -
Multisatellite Determination of the Relativistic Electron Phase Space Density at Geosynchronous Orbit: Methodology and Results During Geomagnetically Quiet Times Y
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 110, A10210, doi:10.1029/2004JA010895, 2005 Multisatellite determination of the relativistic electron phase space density at geosynchronous orbit: Methodology and results during geomagnetically quiet times Y. Chen, R. H. W. Friedel, and G. D. Reeves Los Alamos National Laboratory, Los Alamos, New Mexico, USA T. G. Onsager NOAA, Boulder, Colorado, USA M. F. Thomsen Los Alamos National Laboratory, Los Alamos, New Mexico, USA Received 10 November 2004; revised 20 May 2005; accepted 8 July 2005; published 20 October 2005. [1] We develop and test a methodology to determine the relativistic electron phase space density distribution in the vicinity of geostationary orbit by making use of the pitch-angle resolved energetic electron data from three Los Alamos National Laboratory geosynchronous Synchronous Orbit Particle Analyzer instruments and magnetic field measurements from two GOES satellites. Owing to the Earth’s dipole tilt and drift shell splitting for different pitch angles, each satellite samples a different range of Roederer L* throughout its orbit. We use existing empirical magnetic field models and the measured pitch-angle resolved electron spectra to determine the phase space density as a function of the three adiabatic invariants at each spacecraft. Comparing all satellite measurements provides a determination of the global phase space density gradient over the range L* 6–7. We investigate the sensitivity of this method to the choice of the magnetic field model and the fidelity of the instrument intercalibration in order to both understand and mitigate possible error sources. Results for magnetically quiet periods show that the radial slopes of the density distribution at low energy are positive, while at high energy the slopes are negative, which confirms the results from some earlier studies of this type. -
Positioning: Drift Orbit and Station Acquisition
Orbits Supplement GEOSTATIONARY ORBIT PERTURBATIONS INFLUENCE OF ASPHERICITY OF THE EARTH: The gravitational potential of the Earth is no longer µ/r, but varies with longitude. A tangential acceleration is created, depending on the longitudinal location of the satellite, with four points of stable equilibrium: two stable equilibrium points (L 75° E, 105° W) two unstable equilibrium points ( 15° W, 162° E) This tangential acceleration causes a drift of the satellite longitude. Longitudinal drift d'/dt in terms of the longitude about a point of stable equilibrium expresses as: (d/dt)2 - k cos 2 = constant Orbits Supplement GEO PERTURBATIONS (CONT'D) INFLUENCE OF EARTH ASPHERICITY VARIATION IN THE LONGITUDINAL ACCELERATION OF A GEOSTATIONARY SATELLITE: Orbits Supplement GEO PERTURBATIONS (CONT'D) INFLUENCE OF SUN & MOON ATTRACTION Gravitational attraction by the sun and moon causes the satellite orbital inclination to change with time. The evolution of the inclination vector is mainly a combination of variations: period 13.66 days with 0.0035° amplitude period 182.65 days with 0.023° amplitude long term drift The long term drift is given by: -4 dix/dt = H = (-3.6 sin M) 10 ° /day -4 diy/dt = K = (23.4 +.2.7 cos M) 10 °/day where M is the moon ascending node longitude: M = 12.111 -0.052954 T (T: days from 1/1/1950) 2 2 2 2 cos d = H / (H + K ); i/t = (H + K ) Depending on time within the 18 year period of M d varies from 81.1° to 98.9° i/t varies from 0.75°/year to 0.95°/year Orbits Supplement GEO PERTURBATIONS (CONT'D) INFLUENCE OF SUN RADIATION PRESSURE Due to sun radiation pressure, eccentricity arises: EFFECT OF NON-ZERO ECCENTRICITY L = difference between longitude of geostationary satellite and geosynchronous satellite (24 hour period orbit with e0) With non-zero eccentricity the satellite track undergoes a periodic motion about the subsatellite point at perigee. -
An Introduction to Rockets -Or- Never Leave Geeks Unsupervised
An Introduction to Rockets -or- Never Leave Geeks Unsupervised Kevin Mellett 27 Apr 2006 2 What is a Rocket? • A propulsion system that contains both oxidizer and fuel • NOT a jet, which requires air for O2 3 A Brief History • 400 BC – Steam Bird • 100 BC – Hero Engine • 100 AD – Gunpowder Invented in China – Celebrations – Religious Ceremonies – Bamboo Misfires? 4 A Brief History • Chinese Invent Fire Arrows 13th c – First True Rockets •16th c Wan-Hu – 47 Rockets 5 A Brief History •13th –16th c Improvements in Technology – English Improved Gunpowder – French Improved Guidance by Shooting Through a Tube “Bazooka Style” – Germans Invented “Step Rockets” (Staging) 6 A Brief History • 1687 Newton Publishes Principia Mathematica 7 Newton’s Third Law MOMENTUM is the key concept of rocketry 8 A Brief History • 1903 KonstantineTsiolkovsky Publishes the “Rocket Equation” – Proposes Liquid Fuel ⎛ Mi ⎞ V = Ve*ln⎜ ⎟ ⎝ Mf ⎠ 9 A Brief History • Goddard Flies the First Liquid Fueled Rocket on 16 Mar 1926 – Theorized Rockets Would Work in a Vacuum – NY Times: Goddard “…lacks the basic physics ladeled out in our high schools…” 10 A Brief History • Germans at Peenemunde – Oberth and von Braun lead development of the V-2 – Amazing achievement, but too late to change the tide of WWII – After WWII, USSR and USA took German Engineers and Hardware 11 Mission Requirements • Launch On Need – No Time for Complex Pre-Launch Preps – Long Shelf Life • Commercial / Government – Risk Tolerance –R&D Costs 12 Mission Requirements • Payload Mass and Orbital Objectives – How much do you need, and where do you want it? Both drive energy requirements. -
Derivation of Atmospheric Aerosol and Cloud Parameters from the Satellite Sensors on Board Himawari 8-9, GCOM-C, Earthcare, and GOSAT2 Satellites
9-11 Oct. 2013, Melbourne 4th Asia/Oceania Meteorological Satellite Users' Conference Derivation of atmospheric aerosol and cloud parameters from the satellite sensors on board Himawari 8-9, GCOM-C, EarthCARE, and GOSAT2 satellites Teruyuki Nakajima ([email protected]) Surface solar radiation retrieval (1) PV system malfunction detection 2013 result (2011/7 ) EXAM system: Takenaka et al. (JGR 11) (2) Solar car race support DARWIN World Solar Challenge 3,000 km (WSC) in 2011 Tokai U. team Winner 2011-2012 ADELAIDE 2nd in 2013 HIMAWARI7 Next generation satellites AHI specs, JMA/ HIMAWARI-8/9 2016- 16 bands (1km, 2km) EarthCARE Full disk scan every 10min Rapid scan every 2.5 min 2009-, 2016- Aerosol and cloud GOSAT, GOSAT-II 20- monitoring GCOM-C CGOM/C-SGLI 250m, 11ch Current 2nd generation 500m, 2 ch imager 2015- 3rd generation back/forward view 1km, 4 ch Himawari-8&9 with polarization GOSAT2/FTS-SWIR FTS-TIR CAI2 NASA/ LARC Coarse aerosol correction Imaging Dynamics with aerosol ESA-JAXA/EarthCARE Radar Echo Aerosol forcing XCO2, XCH4 Doppler velocity NASA/LARC JMA Advisory Committee for Geostationary Satellite Data Use Members: T. Nakajima (Chair), R. Oki (JAXA), T. Koike, H. Shimoda, T. Takamura, Y. Takayabu, E. Nakakita, T.Y. Nakajima, K. Nakamura, Y. Honda WGs: T.Y. Nakajima (Atmosphere), Y. Honda (Earth surface) Data use exploitation and community supports Data distributions to research community (430GB/day nc) Algorithm developments and requests from foreign agencies and groups? Simulation data (Himawari -
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................ -
Richard Dalbello Vice President, Legal and Government Affairs Intelsat General
Commercial Management of the Space Environment Richard DalBello Vice President, Legal and Government Affairs Intelsat General The commercial satellite industry has billions of dollars of assets in space and relies on this unique environment for the development and growth of its business. As a result, safety and the sustainment of the space environment are two of the satellite industry‘s highest priorities. In this paper I would like to provide a quick survey of past and current industry space traffic control practices and to discuss a few key initiatives that the industry is developing in this area. Background The commercial satellite industry has been providing essential space services for almost as long as humans have been exploring space. Over the decades, this industry has played an active role in developing technology, worked collaboratively to set standards, and partnered with government to develop successful international regulatory regimes. Success in both commercial and government space programs has meant that new demands are being placed on the space environment. This has resulted in orbital crowding, an increase in space debris, and greater demand for limited frequency resources. The successful management of these issues will require a strong partnership between government and industry and the careful, experience-based expansion of international law and diplomacy. Throughout the years, the satellite industry has never taken for granted the remarkable environment in which it works. Industry has invested heavily in technology and sought out the best and brightest minds to allow the full, but sustainable exploitation of the space environment. Where problems have arisen, such as space debris or electronic interference, industry has taken 1 the initiative to deploy new technologies and adopt new practices to minimize negative consequences. -
The Progress of Fengyun Satellite Program and Its Applications
The Progress of Fengyun Satellite Program and Its Applications Qifeng LU National Satellite Meteorological Center, China Meteorological Administration (NSMC/CMA) United Nations/China Forum on Space Solutions: Realizing the Sustainable Development Goals Outline Fengyun Program Overview Current Missions and Services Latest Progress Future Programs National Satellite Meteorological Center ,CMA 1. Fengyun Program Overview Chinese FENGYUN Meteorological Satellites Polar System Geostationary System First Generation First FY-1 A, B, C, D Generation FY-2 A, B, C, D, E, F, G, H Second Second Generation Generation FY-3 A, B, C, D FY-4 A FY-3E, F, G planned until 2025 FY-4B, C, D planned until 2025 2019/5/3 United Nations/China Forum on Space Solutions: Realizing the Sustainable Development Goals 3 Launched Satellites Since Jan. 1969, China began to develop his own meteorological Satellite Leo Launch Data Geo Launch Data FY-1A Sept. 7, 1988 FY-2A Jun. 10, 1997 FY-1B Sept. 3, 1990 FY-2B Jun. 25, 2000 FY-1C May 10, 1999 FY-2C Oct. 18, 2004 FY-1D May 15, 2002 FY-2D Dec. 8, 2006 FY-3A May 27, 2008 FY-2E Dec. 23, 2008 FY-3B Nov. 5, 2010 FY-2F Jan. 13, 2012 FY-3C Sept. 23, 2013 FY-2G Dec. 31, 2014 FY-3D Nov. 15, 2017 FY-4A Dec. 11, 2016 FY-2H Jun. 5, 2018 Overall Development Strategy (4 stages): 1) 1970 - 1990: Conducting satellite research and development 2) 1990 - 2000: Implementing transition from R&D to operational 3) 2000 - 2010: Implementing transition from 1st generation to 2nd generation 4) 2010 - 2020: Pursuing accuracy and precision of satellite measurements 2019/5/3 United Nations/China Forum on Space Solutions: Realizing the Sustainable Development Goals 4 International User Community Global Data Regional Data Kangerlussu Svalbard aq Lannion MaspalomaAthens s FY-3C sounding data have been assimilated into CMA GRAPES, ECMWF, EUMETSAT Advanced UK NWP model operationally. -
GEO, MEO, and LEO How Orbital Altitude Impacts Network Performance in Satellite Data Services
GEO, MEO, AND LEO How orbital altitude impacts network performance in satellite data services COMMUNICATION OVER SATELLITE “An entire multi-orbit is now well accepted as a key enabler across the telecommunications industry. Satellite networks can supplement existing infrastructure by providing global reach satellite ecosystem is where terrestrial networks are unavailable or not feasible. opening up above us, But not all satellite networks are created equal. Providers offer different solutions driving new opportunities depending on the orbits available to them, and so understanding how the distance for high-performance from Earth affects performance is crucial for decision making when selecting a satellite service. The following pages give an overview of the three main orbit gigabit connectivity and classes, along with some of the principal trade-offs between them. broadband services.” Stewart Sanders Executive Vice President of Key terms Technology at SES GEO – Geostationary Earth Orbit. NGSO – Non-Geostationary Orbit. NGSO is divided into MEO and LEO. MEO – Medium Earth Orbit. LEO – Low Earth Orbit. HTS – High Throughput Satellites designed for communication. Latency – the delay in data transmission from one communication endpoint to another. Latency-critical applications include video conferencing, mobile data backhaul, and cloud-based business collaboration tools. SD-WAN – Software-Defined Wide Area Networking. Based on policies controlled by the user, SD-WAN optimises network performance by steering application traffic over the most suitable access technology and with the appropriate Quality of Service (QoS). Figure 1: Schematic of orbital altitudes and coverage areas GEOSTATIONARY EARTH ORBIT Altitude 36,000km GEO satellites match the rotation of the Earth as they travel, and so remain above the same point on the ground.