Comparison of Aqua/Terra MODIS and Himawari-8 Satellite Data on Cloud Mask and Cloud Type Classification Using Split Window Algorithm
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
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 -
First Provisional Land Surface Reflectance Product From
remote sensing Letter First Provisional Land Surface Reflectance Product from Geostationary Satellite Himawari-8 AHI Shuang Li 1,2, Weile Wang 3, Hirofumi Hashimoto 3 , Jun Xiong 4, Thomas Vandal 4, Jing Yao 1,2, Lexiang Qian 5,*, Kazuhito Ichii 6, Alexei Lyapustin 7 , Yujie Wang 7,8 and Ramakrishna Nemani 9 1 School of Geography and Resources, Guizhou Education University, Guiyang 550018, China; [email protected] (S.L.); [email protected] (J.Y.) 2 Guizhou Provincial Key Laboratory of Geographic State Monitoring of Watershed, Guizhou Education University, Guiyang 550018, China 3 NASA Ames Research Center—California State University Monterey Bay (CSUMB), Moffett Field, CA 94035, USA; [email protected] (W.W.); [email protected] (H.H.) 4 NASA Ames Research Center—Bay Area Environmental Research Institute (BAERI), Moffett Field, CA 94035, USA; [email protected] (J.X.); [email protected] (T.V.) 5 School of Geographical Sciences, Guangzhou University, Guangzhou 510006, China 6 Center for Environmental Remote Sensing, Chiba University, Chiba 263-8522, Japan; [email protected] 7 NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; [email protected] (A.L.); [email protected] (Y.W.) 8 Joint Center for Earth systems Technology (JCET), University of Maryland-Baltimore County (UMBC), Baltimore, MD 21228, USA 9 Goddard Space Flight Center—NASA Ames Research Center, Moffett Field, CA 94035, USA; [email protected] * Correspondence: [email protected] Received: 11 October 2019; Accepted: 2 December 2019; Published: 12 December 2019 Abstract: A provisional surface reflectance (SR) product from the Advanced Himawari Imager (AHI) on-board the new generation geostationary satellite (Himawari-8) covering the period between July 2015 and December 2018 is made available to the scientific community. -
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 -
Aqua: an Earth-Observing Satellite Mission to Examine Water and Other Climate Variables Claire L
IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING, VOL. 41, NO. 2, FEBRUARY 2003 173 Aqua: An Earth-Observing Satellite Mission to Examine Water and Other Climate Variables Claire L. Parkinson Abstract—Aqua is a major satellite mission of the Earth Observing System (EOS), an international program centered at the U.S. National Aeronautics and Space Administration (NASA). The Aqua satellite carries six distinct earth-observing instruments to measure numerous aspects of earth’s atmosphere, land, oceans, biosphere, and cryosphere, with a concentration on water in the earth system. Launched on May 4, 2002, the satellite is in a sun-synchronous orbit at an altitude of 705 km, with a track that takes it north across the equator at 1:30 P.M. and south across the equator at 1:30 A.M. All of its earth-observing instruments are operating, and all have the ability to obtain global measurements within two days. The Aqua data will be archived and available to the research community through four Distributed Active Archive Centers (DAACs). Index Terms—Aqua, Earth Observing System (EOS), remote sensing, satellites, water cycle. I. INTRODUCTION AUNCHED IN THE early morning hours of May 4, 2002, L Aqua is a major satellite mission of the Earth Observing System (EOS), an international program for satellite observa- tions of earth, centered at the National Aeronautics and Space Administration (NASA) [1], [2]. Aqua is the second of the large satellite observatories of the EOS program, essentially a sister satellite to Terra [3], the first of the large EOS observatories, launched in December 1999. Following the phraseology of Y. -
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 ........................................................................................................................ -
Status Report on the Status Report on the Current and Future Satellite
Coordination Group for Meteorological Satellites ‐ CGMS Status report on the current and future satellite systems by JAXA Presented to CGMS-44 Plenary session, agenda item [D.2] Add CGMS agency logo here (in the slide master) Agency, version?, Date 2014? [update filed in the slide master] Coordination Group for Meteorological Satellites ‐ CGMS Overview ‐ Planning of JAXA satellite systems Targets (JFY) 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 2018 Positioning QZS-1 [Land and Disaster monitoring] Disasters & ALOS/PALSAR ALOS-2 PALSAR-2 Resources ALOS Advanced Optical ALOS/PRISM AVNIR2 [Precipitation] Climate Change GPM / DPR TRMM/PR & Water TRMM [Wind, SST , Water vapor] Water Cycle Aqua/AMSR‐E Aqua GCOM-W / AMSR2 [Vegetation, aerosol, cloud, SST, ocean color] 250m, multi‐angle, polarization GCOM-C / SGLI Climate Change [Cloud and Aerosol 3D structure] EarthCARE / CPR Greenhouse [CO2, Methane] [CO2, Methane, CO] gases GOSAT GOSAT-2 ETS-VIII Communication WINDS Add CGMS agency logo here (in the slide master) On orbit Phase C/D Phase A/B Agency, version?, Date 2014? [update filed in the slide master] 2 Coordination Group for Meteorological Satellites ‐ CGMS Earth Observation ‐ ALOS‐2 ‐ GPM/DPR ‐ GCOM‐W/C ‐ GOSAT/GOSAT‐2 ‐ EarthCARE/CPR Add CGMS agency logo here (in the slide master) Agency, version?, Date 2014? [update filed in the slide master] Coordination Group for Meteorological Satellites ‐ CGMS Disaster, Land, Agriclture, Application Natural Resources, Sea Ice & Maritime Safety Stripmap: 3 to 10m res., 50 to 70 km L-band SAR -
Introduction of JMA Himawari Follow-On Satellites Program
Introduction of JMA Himawari follow-on satellites program Himawari-9 Kotaro BESSHO Satellite Program Division Himawari-8 Japan Meteorological Agency Himawari-8/9 Advanced Himawari Imager (AHI) Geostationary Around 140.7°E communication antennas position Attitude control 3-axis attitude-controlled geostationary satellite 1) Raw observation data transmission Ka-band, 18.1 - 18.4 GHz (downlink) 2) DCS (Data collection System) International channel 402.0 - 402.1 MHz (uplink) Domestic channel Communication 402.1 - 402.4 MHz (uplink) solar panel Transmission to ground segments Ka-band, 18.1 - 18.4 GHz (downlink) Himawari-8 began operation on 7 July 3) Telemetry and command 2015, replacing the previous MTSAT-2 Ku-band, 12.2 - 12.75 GHz (downlink) 13.75 - 14.5 GHz (uplink) operational satellite 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 2025 2026 2027 2028 2029 MTSAT-1R operation standby MTSAT-2 standby operation standby Himawari-8 a package manufacture launch operation standby Himawari-9 purchase manufacture launch standby operation standby Himawari-8/-9 follow-on program • 2018: JMA started considering the next GEO satellite program The Implementation Plan of the Basic Plan on Space Policy: “By FY2023 Japan will start manufacturing the Geostationary Meteorological Satellites that will be the successors to Himawari-8 and -9, aiming to put them into operation in around FY2029”. Description of Japan’s geostationary meteorological satellites in the Implementation Plan revised in FY2017 Himawari-8/-9 -
NASA's Aqua and GPM Satellites Examine Tropical Cyclone Kenanga 17 December 2018
NASA's Aqua and GPM satellites examine Tropical Cyclone Kenanga 17 December 2018 northeast of Kenanga's center of circulation was dropping rain at a rate of over 119 mm (4.7 inches) per hour. At NASA's Goddard Space Flight Center in Greenbelt, Maryland, imagery and animations were created using GPM data. A 3-D animation used GPM's radar to show the structure of precipitation within tropical Cyclone Kenanga. The simulated flyby around Kenanga showed storm tops that were reaching heights above 13.5 km (8.4 miles). GPM is a joint mission between NASA and the Japanese space agency JAXA. On Dec. 17 at 3:05 a.m. EST (0805 UTC), NASA's Aqua satellite provided an infrared look at Tropical Cyclone Kenanga. Coldest cloud top temperatures (in purple) indicated where strongest storms appeared. Credit: NASA JPL/Heidar Thrastarson On December 16 and 17, NASA's GPM core observatory satellite and NASA's Aqua satellite, respectively, passed over the Southern Indian Ocean and captured rainfall and temperature data on Tropical Cyclone Kenanga. Kenanga formed on Dec. 15 about 1,116 miles east of Diego Garcia, and strengthened into a tropical storm. When the Global Precipitation Measurement mission or GPM core satellite passed overhead, The GPM core satellite found that a powerful storm the rainfall rates it gathered were derived from the northeast of Kenanga's center of circulation was dropping satellite's Microwave Imager (GMI) instrument. rain at a rate of over 119 mm (4.7 inches) per hour. GPM provided a close-up analysis of rainfall Credit: NASA /JAXA, Hal Pierce around tropical cyclone Kenanga. -
Hi-Reliability Products for Space
Hi-Reliability Products for Space Introduction Rakon is one of the world’s largest solutions providers of high reliability frequency control products. Its high reliability solutions are found in Space, Defence and Industrial applications which require the most stringent performance criteria. This is why many government and commercial programmes use Rakon oscillators across the globe, in systems where high performance is required under the most demanding conditions. Rakon continuously develops state of the art frequency control products at the cutting edge of innovative technology. Industry Contribution Space Product Advantages Ê Rakon has a proven record of taking Space specifications and Ê Rakon space grade oscillators (Flight Models) are designed to creating high reliability and cost effective solutions in order to meet TID of 100 kRad, low dose rate (36 – 360 rad/h) as per meet the most demanding requirements. ESCC22900 and latch-up free up to LET of 60 MeV/mg/cm². Ê Rakon is involved in most of the scientific programmes Ê Rakon is among the top worldwide suppliers of Ultra Stable managed by the European Space Agency (ESA), and has OCXO for Space. The mini-USO (Ultra Stable Oscillator) offers supplied ESA qualified crystals since the 1980s. Rakon a guaranteed frequency stability vs. temperature of 0.1 ppb develops new products & technologies under funding from (-20 to +50°C) and short-term stability (Allan variance) of ESA and CNES (French National Centre for Space Studies). 5E-13 from 1 to 100 seconds. Ê As your strategic frequency control partner, Rakon can provide Ê For Low Earth Orbit (LEO) satellites & constellations, Rakon standard products or customised solutions, ranging from high offers RadHard COTS products (e.g. -
SMEX03 ENVISAT ASAR Data, Alabama, Georgia, Oklahoma, Version 1 USER GUIDE
SMEX03 ENVISAT ASAR Data, Alabama, Georgia, Oklahoma, Version 1 USER GUIDE How to Cite These Data As a condition of using these data, you must include a citation: Jackson, T., R. Bindlish, and R. Van der Velde. 2009. SMEX03 ENVISAT ASAR Data, Alabama, Version 1. [Indicate subset used]. Boulder, Colorado USA. NASA National Snow and Ice Data Center Distributed Active Archive Center. doi: https://doi.org/10.5067/7ZGTHVZFAIDT. [Date Accessed]. Jackson, T., R. Bindlish, and R. Van der Velde. 2013. SMEX03 ENVISAT ASAR Data, Georgia, Version 1. [Indicate subset used]. Boulder, Colorado USA. NASA National Snow and Ice Data Center Distributed Active Archive Center. doi: https://doi.org/10.5067/M28ZA9EYPHQ5. [Date Accessed]. Jackson, T., R. Bindlish, and R. Van der Velde. 2013. SMEX03 ENVISAT ASAR Data, Oklahoma, Version 1. [Indicate subset used]. Boulder, Colorado USA. NASA National Snow and Ice Data Center Distributed Active Archive Center. doi: https://doi.org/10.5067/YXYV5M9B6I1J. [Date Accessed]. FOR QUESTIONS ABOUT THESE DATA, CONTACT [email protected] FOR CURRENT INFORMATION, VISIT https://nsidc.org/data/NSIDC-0357, https://nsidc.org/data/NSIDC-0576, https://nsidc.org/data/NSIDC-0577 USER GUIDE: SMEX03 ENVISAT ASAR Data, Alabama, Georgia, Oklahoma, Version 1 TABLE OF CONTENTS 1 DETAILED DATA DESCRIPTION ............................................................................................... 2 1.1 Format .................................................................................................................................................. -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology