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AATSR Frequently Asked Questions (FAQ)
AATSR Frequently Asked Questions (FAQ) Author : IDEAS+ AATSR QC Team (Telespazio VEGA UK) IDEAS+-VEG-OQC-REP-2117 Issue 3 14 December 2016 AATSR Frequently Asked Questions (FAQ) Issue 3 AMENDMENT RECORD SHEET The Amendment Record Sheet below records the history and issue status of this document. ISSUE DATE REASON 1 20 Dec 2005 Initial Issue (as AEP_REP_001) 2 02 Oct 2013 Updated with new questions and information (issued as IDEAS- VEG-OQC-REP-0955) 3 14 Dec 2016 General updates, major edits to Q37., new questions: Q17., Q25., Q26., Q28., Q32., Q38., Q39., Q48. Now issued as IDEAS+-VEG-OQC-REP-2117 TABLE OF CONTENTS 1. INTRODUCTION ........................................................................................................................ 5 1.1 The Third AATSR Reprocessing Dataset (IPF 6.05) ............................................................ 5 1.2 References ............................................................................................................................ 6 2. GENERAL QUESTIONS ........................................................................................................... 7 Q1. What does AATSR stand for? ........................................................................................ 7 Q2. What is AATSR and what does it do? ............................................................................ 7 Q3. What is Envisat? ............................................................................................................. 7 Q4. What orbit does Envisat use? ........................................................................................ -
In Brief Modified to Increase Engine Reliability
r bulletin 102 — may 2000 3rd Space Station ESA, together with a European industrial Element to be Launched consortium headed by DaimlerChrysler (D) and including Belgian, Dutch and French NASA and the Russian Aviation and partners, was responsible for the design, Space Agency (Rosaviakosmos) plan that development and delivery of the core data the next component of the International management system, which provides Space Station (ISS) – the Zvezda service Zvezda’s main computer. module – will be launched on 12 July from the Baikonur Cosmodrome in Kazakhstan. ESA also has a contract with Rosaviakosmos and RSC-Energia for Following a Joint Programme Review and performing system and interface a General Designers’ Review in Moscow, it integration tasks required for docking with was agreed that Zvezda (Russian for Zvezda by ESA’s Automated Transfer ‘star’) will be launched by a Proton rocket Vehicle (ATV), which will be used for ISS with the second and third stage engines re-boost and logistics support missions In Brief modified to increase engine reliability. from 2003 onwards. Through its ATV industrial consortium led by Aerospatiale Zvezda will provide the early living quarters Matra Lanceurs (F), ESA is also procuring for ISS crew, together with the life sup- some Russian hardware and software for port, electrical power distribution, data use with the ATV. management, flight control, and propul- sion systems for the ISS. On the scientific side, ESA has concluded contracts with Rosaviakosmos and RSC- Energia for the conduct of scientific experiments on Zvezda, including the Global Timing System (GTS) and a radiobiology experiment (called Matroshka) to monitor and analyse radiation doses in ISS crew. -
Gnc 2021 Abstract Book
GNC 2021 ABSTRACT BOOK Contents GNC Posters ................................................................................................................................................... 7 Poster 01: A Software Defined Radio Galileo and GPS SW receiver for real-time on-board Navigation for space missions ................................................................................................................................................. 7 Poster 02: JUICE Navigation camera design .................................................................................................... 9 Poster 03: PRESENTATION AND PERFORMANCES OF MULTI-CONSTELLATION GNSS ORBITAL NAVIGATION LIBRARY BOLERO ........................................................................................................................................... 10 Poster 05: EROSS Project - GNC architecture design for autonomous robotic On-Orbit Servicing .............. 12 Poster 06: Performance assessment of a multispectral sensor for relative navigation ............................... 14 Poster 07: Validation of Astrix 1090A IMU for interplanetary and landing missions ................................... 16 Poster 08: High Performance Control System Architecture with an Output Regulation Theory-based Controller and Two-Stage Optimal Observer for the Fine Pointing of Large Scientific Satellites ................. 18 Poster 09: Development of High-Precision GPSR Applicable to GEO and GTO-to-GEO Transfer ................. 20 Poster 10: P4COM: ESA Pointing Error Engineering -
Real-Time On-Orbit Calibration of Angles Between Star Sensor and Earth Observation Camera for Optical Surveying and Mapping Satellites
ISPRS Annals of the Photogrammetry, Remote Sensing and Spatial Information Sciences, Volume IV-2/W5, 2019 ISPRS Geospatial Week 2019, 10–14 June 2019, Enschede, The Netherlands REAL-TIME ON-ORBIT CALIBRATION OF ANGLES BETWEEN STAR SENSOR AND EARTH OBSERVATION CAMERA FOR OPTICAL SURVEYING AND MAPPING SATELLITES Wei Liu 1*, Hui Wang 2, Weijiao Jiang 2, Fangming Qian 3, Leiming Zhu 4 1 Xi’an Research Institute of Surveying and Mapping, No.1 Middle Yanta Road, Xi’an, China - [email protected] 2 State Key Laboratory of Integrated Service Network, Xidian University, Xi’an, China - [email protected] 2 State Key Laboratory of Integrated Service Network, Xidian University, Xi’an, China - [email protected] 3 Information Engineering University, Zhengzhou, China - [email protected] 4 Centre of TH-Satellite of China, Beijing, China - [email protected] Commission I, WG I/4 KEY WORDS: Star Sensor, Attitude Measurement, Error Analysis, On-Orbit Calibration, Angle between Cameras, On-orbit Monitoring Device ABSTRACT: On space remote sensing stereo mapping field, the angle variation between the star sensor’s optical axis and the earth observation camera’s optical axis on-orbit affects the positioning accuracy, when optical mapping is without ground control points (GCPs). This work analyses the formation factors and elimination methods for both the star sensor’s error and the angles error between the star sensor’s optical axis and the earth observation camera’s optical axis. Based on that, to improve the low attitude stability and long calibration time necessary of current satellite cameras, a method is then proposed for real-time on-orbit calibration of the angles between star sensor’s optical axis and the earth observation camera’s optical axis based on the principle of auto-collimation. -
Space Policy Directive 1 New Shepard Flies Again 5
BUSINESS | POLITICS | PERSPECTIVE DECEMBER 18, 2017 INSIDE ■ Space Policy Directive 1 ■ New Shepard fl ies again ■ 5 bold predictions for 2018 VISIT SPACENEWS.COM FOR THE LATEST IN SPACE NEWS INNOVATION THROUGH INSIGNT CONTENTS 12.18.17 DEPARTMENTS 3 QUICK TAKES 6 NEWS Blue Origin’s New Shepard flies again Trump establishes lunar landing goal 22 COMMENTARY John Casani An argument for space fission reactors 24 ON NATIONAL SECURITY Clouds of uncertainty over miltary space programs 26 COMMENTARY Rep. Brian Babin and Rep. Ami Ber We agree, Mr. President,. America should FEATURE return to the moon 27 COMMENTARY Rebecca Cowen- 9 Hirsch We honor the 10 Paving a clear “Path” to winners of the first interoperable SATCOM annual SpaceNews awards. 32 FOUST FORWARD Third time’s the charm? SpaceNews will not publish an issue Jan. 1. Our next issue will be Jan. 15. Visit SpaceNews.com, follow us on Twitter and sign up for our newsletters at SpaceNews.com/newsletters. ON THE COVER: SPACENEWS ILLUSTRATION THIS PAGE: SPACENEWS ILLUSTRATION FOLLOW US @SpaceNews_Inc Fb.com/SpaceNewslnc youtube.com/user/SpaceNewsInc linkedin.com/company/spacenews SPACENEWS.COM | 1 VOLUME 28 | ISSUE 25 | $4.95 $7.50 NONU.S. CHAIRMAN EDITORIAL CORRESPONDENTS ADVERTISING SUBSCRIBER SERVICES Felix H. Magowan EDITORINCHIEF SILICON VALLEY BUSINESS DEVELOPMENT DIRECTOR TOLL FREE IN U.S. [email protected] Brian Berger Debra Werner Paige McCullough Tel: +1-866-429-2199 Tel: +1-303-443-4360 [email protected] [email protected] [email protected] Fax: +1-845-267-3478 +1-571-356-9624 Tel: +1-571-278-4090 CEO LONDON OUTSIDE U.S. -
Outstanding Expertise at the Service of Your Ambitions
OUTSTANDING EXPERTISE AT THE SERVICE OF YOUR AMBITIONS #enablingyourambitions MILLION TURNOVER IN 2017 ambitions your EMPLOYEES INCLUDING ING 60% ENGINEERS OUR GOAL: L 70+ TO COMBINE‘‘ ENAB TECHNOLOGICAL EXCELLENCE AND 360 COMPETITIVENESS SODERN TO TRANSFORM OUR CUSTOMERS’ AMBITIONS 2 INTO REALITIES.‘‘ OUR DNA Franck Poirrier, CEO of Sodern We rely on more than 50 years of experience sharehoLDers: ArianeGroUP (90%) in optronics and neutron technology AND CEA (10%) 16600 to develop innovative and competitive solutions for our commercial and institutional customers. M2 OF FACILITIES 2 KEY AREAS As a subsidiary of the We preserve and enhance To meet the expectations of OF KNOW-HOW: European leader in access this exceptional technological changing markets, we set high OPTRONIC, to space, ArianeGroup, know-how by participating in competitive requirements for NEUtron we are operationally scientific programs that push ourselves: the implementation technoLOGY independent. the limits of the state of the of lean management, perfect art: the caesium atom clock understanding of our We are also a historical and Pharao, the seismometer of customers’ needs, agility and strategic defence supplier, a the Mars mission InSight, cells optimisation of production characteristic that guarantees of Pockels for the Megajoule costs are the commitments us a solid base of industrial laser, etc. that allow us to maintain a activities, thereby affirming competitive edge with a very durability and reliability. Sodern’s core business is the high level of customer Our institutional clients’ high series production of star satisfaction, and to consolidate level of requirements has led trackers that enable satellites our position as a world leader us to develop an extraordinary to orient themselves precisely in in several markets. -
FAME-C: Cloud Property Retrieval Using Synergistic AATSR and MERIS Observations
Atmos. Meas. Tech., 7, 3873–3890, 2014 www.atmos-meas-tech.net/7/3873/2014/ doi:10.5194/amt-7-3873-2014 © Author(s) 2014. CC Attribution 3.0 License. FAME-C: cloud property retrieval using synergistic AATSR and MERIS observations C. K. Carbajal Henken, R. Lindstrot, R. Preusker, and J. Fischer Institute for Space Sciences, Freie Universität Berlin (FUB), Berlin, Germany Correspondence to: C. K. Carbajal Henken ([email protected]) Received: 29 April 2014 – Published in Atmos. Meas. Tech. Discuss.: 19 May 2014 Revised: 17 September 2014 – Accepted: 11 October 2014 – Published: 25 November 2014 Abstract. A newly developed daytime cloud property re- trievals. Biases are generally smallest for marine stratocu- trieval algorithm, FAME-C (Freie Universität Berlin AATSR mulus clouds: −0.28, 0.41 µm and −0.18 g m−2 for cloud MERIS Cloud), is presented. Synergistic observations from optical thickness, effective radius and cloud water path, re- the Advanced Along-Track Scanning Radiometer (AATSR) spectively. This is also true for the root-mean-square devia- and the Medium Resolution Imaging Spectrometer (MERIS), tion. Furthermore, both cloud top height products are com- both mounted on the polar-orbiting Environmental Satellite pared to cloud top heights derived from ground-based cloud (Envisat), are used for cloud screening. For cloudy pixels radars located at several Atmospheric Radiation Measure- two main steps are carried out in a sequential form. First, ment (ARM) sites. FAME-C mostly shows an underestima- a cloud optical and microphysical property retrieval is per- tion of cloud top heights when compared to radar observa- formed using an AATSR near-infrared and visible channel. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Sentinel-1A Launch
SENTINEL-1A LAUNCH Arianespace’s seventh Soyuz launch from the Guiana Space Center will orbit Sentinel-1A, the first satellite in Europe’s Earth observation program, Copernicus. The European Space Agency (ESA) chose Thales Alenia Space to design, develop and build the satellite, as well as perform related tests. Copernicus is the new name for the European program previously known as GMES (Global Monitoring for Environment and Security), and is the European Commission’s second major space program, following Galileo. Copernicus is designed to give Europe continuous, independent and reliable access to Earth observation data. With the Soyuz, Ariane 5 and Vega launchers at the Guiana Space Center (CSG), Arianespace is the only launch services provider in the world capable of launching all types of payloads into all orbits, from the smallest to the largest geostationary satellites, from satellite clusters for constellations to cargo missions for the International Space Station (ISS). Arianespace sets the launch services standard for all operators, whether commercial or governmental, and guarantees access to space for scientific missions. Sentinel-1A is the 50th satellite with an Earth observation payload to be launched by Arianespace. Arianespace has seven more Earth observation missions in its order book, including four commercial missions (signed in 2013 and 2014). The Copernicus program is designed to give Europe complete independence in the acquisition and management of environmental data concerning our planet. ESA’s Sentinel programs comprise five satellite families: Sentinel-1, to provide continuity for radar data from ERS and Envisat. Sentinel-2 and Sentinel-3, dedicated to the observation of the Earth and its oceans. -
Metop Second Generation Payload
MetOp Second Generation Payload Marc Loiselet, Ville Kangas, Ilias Manolis, Franco Fois, Salvatore d’Addio European Space Agency, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands E-mail: [email protected] MetOp-Second Generation Satellite Instruments Instrument Provider The ESA MetOp Second Generation (MetOp-SG) Programme was approved at the ESA Council Meeting at Ministerial level in Naples in Sat-A METimage DLR via EUMETSAT November 2012. IASI-NG CNES via EUMETSAT MetOp-SG is a follow-on to the current, first generation series of MetOp satellites, which is now established as a cornerstone of the global MWS ESA – MetOp-SG network of meteorological satellites. RO ESA – MetOp-SG The MetOp-SG programme is being implemented in collaboration with EUMETSAT. 3MI ESA – MetOp-SG ESA will develop the prototype MetOp-SG satellites (including associated instruments) and procure, on behalf of EUMETSAT, the recurrent Sentinel-5 ESA – GMES satellites (and associated instruments). The overall MetOp-SG space segment architecture consists of two series of satellites (Sat-A, Sat-B), each carrying different suites of instruments and operating in LEO polar orbit. The planned launches of the first of each series of satellites Sat-B SCA ESA – MetOp-SG are at the beginning of 2021 and at end 2022, respectively. MWI ESA – MetOp-SG RO ESA – MetOp-SG More information can be found in the “MetOp Second Generation – Overview” presentation from Graeme Mason, Hubert Barré, Maurizio ICI ESA – MetOp-SG Betto, ESA-ESTEC, The Netherlands. Argos-4 CNES via EUMETSAT Payload ESA is responsible for instrument design of six instruments, namely the MicroWave Sounder (MWS), Scatterometer (SCA), the Radio Occultation (RO), the MicroWave Imaging (MWI), the Ice Cloud Imager (ICI), and the Multi-viewing, Multi-channel, Multi-polarisation imager (3MI). -
IASI: a Review of Instrument Performance and Characterizations
IASI: a Review of Instrument Performance and Characterizations D. Siméonia, D. Blumsteinb, P. Astruca, C. Degrellea, B. Chetritea, B. Tournierd, G. Chalonb, T. Carlierb, G. Kayalc a ALCATEL SPACE -10 Bd du Midi BP99-06156 Cannes La Bocca Cedex - France, b CNES - 18 avenue Edouard Belin – 31401 Toulouse Cedex 9 – France c EUMETSAT – Am Kavalleriesant 31, D-64295 Darmstadt – Germany d NOVELTIS-Parc Tech du Canal – 2, av. de l’Europe – 31526 Ramonville St Agne Cedex-France Corporate Communications IASI Payload of the European Meteorological Polar-Orbit Satellites METOP Mains missions: weather predictions and climate studies. Program led by the French National Space Agency CNES in association with the European Meteorological Satellite Organization EUMETSAT. Prime Contractor: Thales Alenia Space Dimensions of sounder : 1.1x1.1x1.2 m3 Mass sounder < 200 Kg Stiffness > 55Hz during launch Power consumption < 200 Watt Reliability > 0.8 Availability > 97.5 % over 5 years 2 All rights reserved © 2007, Thales Alenia Space IASI Payload of the European Meteorological Polar-Orbit Satellites METOP Mains missions: weather predictions and climate studies. Program led by the French National Space Agency CNES in association with the European Meteorological Satellite Organization EUMETSAT. Prime Contractor: Thales Alenia Space Dimensions of sounder : 1.1x1.1x1.2 m3 Mass sounder < 200 Kg Stiffness > 55Hz during launch Power consumption < 200 Watt Reliability > 0.8 Availability > 97.5 % over 5 years Status : - EM delivered in Dec 2001 - PFM delivered in July -
Sentinel-3 Product Notice
Copernicus S3 Product Notice – Altimetry Mission S3 Sensor SRAL / MWR Product LAND L2 NRT, STC and NTC Product Notice ID S3A.PN-STM-L2L.10 Issue/Rev Date 16/07/2020 Version 1.1 This Product Notice was prepared by the S3 Mission Performance Centre Preparation and ESA experts Approval ESA Mission Management Summary This is a Product Notice (PN) for the Copernicus Sentinel-3A and Sentinel-3B Surface Topography Mission (STM) Level-2 Land products at Near Real Time (NRT), Short Time Critical (STC) and Non Time Critical (NTC) timeliness. The Notice describes the STM current status, product quality and limitations, and product availability status. © ESA page 1 / 16 Processing Baseline S3A S3B Processing Baseline • Processing Baseline: 2.68 • Processing Baseline: 1.42 • • SR_1 IPF version: 06.18 SR_1 IPF version: 06.18 • MW_1 IPF version: 06.11 IPFs version • MW_1 IPF version: 06.11 • • SM_2 IPF version: 06.19 SM_2 IPF version: 06.19 Current Operational Processing Baseline IPF IPF Version In OPE since S3A SR1 06.18 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3A MW1 06.11 Land Centres: NRT mode : 2020-01-21 STC mode : 2020-01-21 NTC mode : 2020-01-21 S3A SM2 06.19 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3B SR1 06.18 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 S3B MW1 06.11 Land Centres: NRT mode : 2020-01-21 STC mode : 2020-01-21 NTC mode : 2020-01-21 S3B SM2 06.19 Land Centres: NRT mode : 2020-07-09 STC mode : 2020-07-09 NTC mode : 2020-07-09 © ESA page 2 / 16 Status of the Processing Baseline S3A The Processing Baseline (PB) for Copernicus Sentinel-3A STM products associated to this PN is reported above.