Accuracy of Vaisala RS41 and RS92 Upper Tropospheric Humidity Compared to Satellite Hyperspectral Infrared Measurements
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New Capabilities for All-Weather Microwave Atmospheric Sensing Using Cubesats and Constellations
SSC18-II-07 New Capabilities for All-Weather Microwave Atmospheric Sensing Using CubeSats and Constellations W. Blackwell, K. Clark, D. Cousins, D. Crompton, A. Cunningham, M. Diliberto, L. Fuhrman, R. Leslie, I. Osaretin, and S. Michael MIT Lincoln Laboratory [email protected] ABSTRACT Three MIT Lincoln Laboratory nanosatellite missions flying microwave radiometers for high-resolution atmospheric sensing are in varying stages of development. Microwave instrumentation is particularly well suited for implementation on a very small satellite, as the sensor requirements for power, pointing, and spatial resolution (aperture size) can be accommodated by a nanosatellite platform. The Microsized Microwave Atmospheric Satellite Version 2a (MicroMAS-2a), launched on January 11, 2018 and has demonstrated temperature sounding using channels near 118 GHz and humidity sounding using channels near 183 GHz. A second MicroMAS-2 flight unit (MicroMAS-2b) will be launched in Fall 2018 as part of ELANA-XX. The Time-Resolved Observations of Precipitation structure and storm Intensity with a Constellation of Smallsats (TROPICS) mission was selected by NASA in 2016 as part of the Earth Venture–Instrument (EVI-3) program. The overarching goal for TROPICS is to provide nearly all-weather observations of 3-D temperature and humidity, as well as cloud ice and precipitation horizontal structure, at high temporal resolution to conduct high-value science investigations of tropical cyclones. TROPICS will provide rapid-refresh microwave measurements (median refresh rate of approximately 40 minutes for the baseline mission) over the tropics that can be used to observe the thermodynamics of the troposphere and precipitation structure for storm systems at the mesoscale and synoptic scale over the entire storm lifecycle. -
Innovative Mini Ultralight Radioprobes to Track Lagrangian Turbulence Fluctuations Within Warm Clouds: Electronic Design
sensors Article Innovative Mini Ultralight Radioprobes to Track Lagrangian Turbulence Fluctuations within Warm Clouds: Electronic Design Miryam E. Paredes Quintanilla 1,* , Shahbozbek Abdunabiev 1, Marco Allegretti 1, Andrea Merlone 2 , Chiara Musacchio 2 , Eros G. A. Pasero 1, Daniela Tordella 3 and Flavio Canavero 1 1 Politecnico di Torino, Department of Electronics and Telecommunications (DET), Corso Duca Degli Abruzzi 24, 10129 Torino, Italy; [email protected] (S.A.); [email protected] (M.A.); [email protected] (E.G.A.P.); fl[email protected] (F.C.) 2 Istituto Nazionale di Ricerca Metrologica, Str. Delle Cacce, 91, 10135 Torino, Italy; [email protected] (A.M.); [email protected] (C.M.) 3 Politecnico di Torino, Department of Applied Science and Technology (DISAT), Corso Duca Degli Abruzzi 24, 10129 Torino, Italy; [email protected] * Correspondence: [email protected] Abstract: Characterization of dynamics inside clouds remains a challenging task for weather forecast- ing and climate modeling as cloud properties depend on interdependent natural processes at micro- and macro-scales. Turbulence plays an important role in particle dynamics inside clouds; however, turbulence mechanisms are not yet fully understood partly due to the difficulty of measuring clouds at the smallest scales. To address these knowledge gaps, an experimental method for measuring the influence of small-scale turbulence in cloud formation in situ and producing an in-field cloud Citation: Paredes Quintanilla, M.E.; Lagrangian dataset is being developed by means of innovative ultralight radioprobes. This paper Abdunabiev, S.; Allegretti, M.; presents the electronic system design along with the obtained results from laboratory and field exper- Merlone, A.; Musacchio, C.; Pasero, ≈ ≈ E.G.A.; Tordella, D.; Canavero, F. -
Outcome Budget of the Department of Space Government of India 2013-2014 Contents
OUTCOME BUDGET OF THE DEPARTMENT OF SPACE GOVERNMENT OF INDIA 2013-2014 CONTENTS Page Nos. Executive Summary (i) - (ii) Introduction (Organisational Set-up, Major Projects/ Programmes of Department of Space, Overview Chapter I of 12th Five Year Plan 2012-2017 proposals, 1-13 Mandate and Policy framework of Department of Space) Chapter II Outcome Budget 2013-2014 15-60 Chapter III Reform measures and Policy initiatives 61-62 Review of Performance of the Major ongoing Chapter IV 63-102 Projects/Programmes/Centres of DOS/ISRO Chapter V Financial Review 103-110 Chapter VI Autonomous Bodies of DOS/ISRO 111-119 Annexure Major Indian Space Missions EXECUTIVE SUMMARY i. The primary objective of the Indian Space Programme is to achieve self-reliance in Space Technology and to evolve application programme to meet the developmental needs of the country. Towards meeting this objective, two major operational space systems have been established – the Indian National Satellite (INSAT) for telecommunication, television broadcasting and meteorological service and the Indian Remote Sensing Satellite (IRS) for natural resource monitoring and management. Two operational launch vehicles, Polar Satellite Launch Vehicle (PSLV) and Geosynchronous Satellite Launch Vehicle (GSLV) provide self reliance in launching IRS & INSAT Satellites respectively. ii. The Department of Space (DOS) and the Space Commission was set up in 1972 to formulate and implement Space policies and programmes in the country. The Indian Space Research Organisation (ISRO) is the research and development wing of the Department of Space and is responsible for executing the programmes and schemes of the Department in accordance with the directives and policies laid down by the Space Commission and the DOS. -
The Development of the Atmospheric Measurements by Ultra-Light Spectrometer (AMULSE) Greenhouse Gas Profiling System and Applica
Atmos. Meas. Tech., 13, 3099–3118, 2020 https://doi.org/10.5194/amt-13-3099-2020 © Author(s) 2020. This work is distributed under the Creative Commons Attribution 4.0 License. The development of the Atmospheric Measurements by Ultra-Light Spectrometer (AMULSE) greenhouse gas profiling system and application for satellite retrieval validation Lilian Joly1, Olivier Coopmann2, Vincent Guidard2, Thomas Decarpenterie1, Nicolas Dumelié1, Julien Cousin1, Jérémie Burgalat1, Nicolas Chauvin1, Grégory Albora1, Rabih Maamary1, Zineb Miftah El Khair1, Diane Tzanos2, Joël Barrié2, Éric Moulin2, Patrick Aressy2, and Anne Belleudy2 1GSMA, UMR CNRS 7331, U.F.R. Sciences Exactes et Naturelles, Université de Reims, Reims, France 2CNRM, Université de Toulouse, Météo-France, CNRS, Toulouse, France Correspondence: Lilian Joly ([email protected]) and Olivier Coopmann ([email protected]) Received: 3 September 2019 – Discussion started: 25 September 2019 Revised: 4 April 2020 – Accepted: 22 April 2020 – Published: 12 June 2020 Abstract. We report in this paper the development of an em- files from the assimilation of infrared satellite observations. bedded ultralight spectrometer ( < 3 kg) based on tuneable The results show that the simulations of infrared satellite ob- diode laser absorption spectroscopy (with a sampling rate of servations from IASI (Infrared Atmospheric Sounding Inter- 24 Hz) in the mid-infrared spectral region. This instrument is ferometer) and CrIS (Cross-track Infrared Sounder) instru- dedicated to in situ measurements of the vertical profile con- ments performed in operational mode for numerical weather centrations of three main greenhouse gases – carbon dioxide prediction (NWP) by the radiative transfer model (RTM) RT- (CO2), methane (CH4) and water vapour (H2O) – via stan- TOV (Radiative Transfer for the TIROS Operational Ver- dard weather and tethered balloons. -
Envisat GO MOS an Instrument for Global Atmospheric Ozone Monitoring
SP-1244 ~·f~ esa_=··===+••· ··llll-l'.11~·----·-•• D Envisat GO MOS An Instrument for Global Atmospheric Ozone Monitoring European Space Agency Agence spatiale europeenne SP-1244 May 2001 Envisat GO MOS An Instrument for Global Atmospheric Ozone Monitoring European Space Agency Agence spatiale europeenne Short Title: SP-1244 'Envisat - GOMOS' Published by: ESA Publications Division ESTEC, P.O. Box 299 2200 AG Noordwijk The Netherlands Tel: +31 71 565 3400 Fax: +31 71 565 5433 Technical Coordinators: C. Readings & T. Wehr Editor. R.A. Harris Layout: Isabel Kenny Copyright: © European Space Agency 2001 Price: 30 Euros ISBN No: 92-9092-5 72-8 Printed in: The Netherlands ii Foreword This report is one of a series being <http://envisat.estec.esa.nl>. published to help publicise the A full listing of all the products European Space Agency's planned to be made available shortly environmental research satellite after the end of the commissioning Envisat, which is due to be launched phase (six months after launch) can be in the year 2001. It is intended to found in [ESA l 998b]. support the preparation of the Earth Observation community to utilise the The principal authors of this report measurements of the GOMOS are: (Global Ozone Monitoring by Occultation of Stars) instrument, J.-L. Bertaux, F. Dalaudier and which forms an important part of the A. Hauchecorne of the Service Envisat payload. The heritage of the dAeronomie du CNRS, Verrieres• GOMOS instrument is outlined here le-Buisson, France, M. Chipperfield and its scientific objectives, of the University of Leeds, Leeds, instrument concept, technical UK, D. -
Instrument Intercomparison – Paul Simona 1 DRAGON ADVANCED TRAINING COURSE in ATMOSPHERE REMOTE SENSING Atmospheric Remote Sensing Measurements
DRAGON ADVANCED TRAINING COURSE IN ATMOSPHERE REMOTE SENSING 4. Satellite Validation Principle C o r r e l a t i v e D a t Day 4 Lecture 2 Instrument intercomparison – Paul Simona 1 DRAGON ADVANCED TRAINING COURSE IN ATMOSPHERE REMOTE SENSING Atmospheric Remote Sensing Measurements • Atmosphere is continuously changing in time and space. => No repeated measurements of the same quantity. • Radiation field measurements are direct, all other are indirect • Measurements probe large atmospheric volume => Large averaging and validation by in situ measurements difficult Courtesy Erkki Kyrola Day 4 Lecture 2 Instrument intercomparison – Paul Simon 2 DRAGON ADVANCED TRAINING COURSE IN ATMOSPHERE REMOTE SENSING Atmospheric Satellite Sensors We launch a satellite sensor for dedicated purposes: Meteorology, dynamical tracer, surface UV monitoring; Global climatology; Montreal and Kyoto Protocol related issues; Atmospheric processes: polar chemistry, etc.; Tropospheric issues like pollution, biomass burning, oxidizing capacity…; Radiative Transfer and Chemical Transport modelling. Day 4 Lecture 2 Instrument intercomparison – Paul Simon 3 DRAGON ADVANCED TRAINING COURSE IN ATMOSPHERE REMOTE SENSING Satellite Validation Principles Ideally, the observations of atmospheric constituents must not be dependent on: ¾ the atmospheric temperature; ¾ the abundance of other species; ¾ the Sun elevation; ¾ the presence of clouds; ¾ the instrument degradation (aging); ¾ etc… Day 4 Lecture 2 Instrument intercomparison – Paul Simon 4 DRAGON ADVANCED TRAINING -
Helsinki University of Technology
Aalto University School of Science Degree Programme in Industrial Engineering and Management Timo Tuomivirta Energy management in neighbourhoods Master’s Thesis Espoo, 07/06/2016 Supervisor: Professor Jan Holmström Instructor: M.Sc. Olli Nummelin Title of thesis Energy management in neighbourhoods Degree programme Industrial Engineering and Management Major Industrial Management Code of major TU-22 Supervisor Professor Jan Holmström Thesis advisor M.Sc. Jan Holmström Date 07.06.2016 Number of pages 115+67 Language English The topic of the thesis was to structure, refine, combine, analyse, and model data from real estate. Possibilities to adjust the relationship of utilities demand and supply were evaluated. The information collected from real estate was composed of real estate level and apartment level data. Real estate level data included weather, heating circuit, cooling circuit and domestic water. The apartment level data included room temperature switch, room operating panel and domestic hot-, and cold water consumption. The apartment specific data were aggregated on real estate level. First the interrelation of sub meters and utility companies billing were formed. After that the differences between measurements and company billing were evaluated. Then system specifically on certain time resolution the temperature of supply and return water, electricity consumption, heat energy consumption and cool energy consumption were determined. Hot water, cold water and overall water consumption on certain time resolution were determined. Furthermore, the seasonal ratio of hot and cold water was evaluated. From cold water station related data sample width specific energy efficiency ratio were calculated. From room temperature switch and room operating panel real estate level analysis were aggregated. -
The Technologies That Could Prevent More Mysteries Like That of Missing Malaysia Airlines Flight 370 Page 20
July-August 2014 The technologies that could prevent more mysteries like that of missing Malaysia Airlines Flight 370 Page 20 Hypersonics after WaveRider p.10 40 tons on a dime at Mars p. 36 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AIAA Progress in Astronautics and Aeronautics AIAA’s popular book series Progress in Astronautics and Aeronautics features books that present a particular, well- defi ned subject refl ecting advances in the fi elds of aerospace science, engineering, and/or technology. POPULAR TITLES Tactical and Strategic Missile Guidance, Sixth Edition Paul Zarchan 1026 pages This best-selling title provides an in-depth look at tactical and strategic missile guidance using common language, notation, and perspective. The sixth edition includes six new chapters on topics related to improving missile guidance system performance and understanding key design concepts and tradeoffs. ISBN: 978-1-60086-894-8 List Price: $134.95 “AIAA Best Seller” AIAA Member Price: $104.95 Morphing Aerospace Vehicles and Structures John Valasek 286 pages Morphing Aerospace Vehicles and Structures is a synthesis of the relevant disciplines and applications involved in the morphing of fi xed wing fl ight vehicles. The book is organized into three major sections: Bio-Inspiration; Control and Dynamics; and Smart Materials and Structures. Most chapters are both tutorial and research-oriented in nature, covering elementary concepts through advanced – and in many cases novel – methodologies. ISBN: 978-1-60086-903-7 “Features the -
(NUCAPS): Algorithm Theoretical Basis Documentation
The NOAA Unique CrIS/ATMS Processing System (NUCAPS): Algorithm Theoretical Basis Documentation Prepared by Antonia Gambacorta [email protected] NOAA Center for Weather and Climate Prediction (NCWCP) 5830 University Research Court 2nd Floor, Office 2684 College Park, MD 20740-3818 USA phone: 301-613-3539 Version 1.0 August 21, 2013 Contents 1 Introduction 1 1.1 References . 2 2 Satellite instrument Description 3 2.1 The Advanced Technology Microwave Sounder (ATMS) . 3 2.2 The Cross-Track Infrared Sounder (CrIS) . 3 2.3 References . 4 3 Algorithm Description 5 3.1 References . 5 4 Algorithm Inputs 7 4.1 Background Climatology Look Up Tables . 7 4.2 Local Angle Adjustment Coefficients . 8 4.3 Forecast Surface Pressure . 8 4.4 Surface Emissivity First Guess . 8 4.5 Microwave and Infrared Tuning Coefficients . 8 4.6 The Radiative Transfer Model . 10 4.6.1 Radiative Transfer Model of the Atmosphere in the Microwave . 11 4.6.2 Radiative Transfer Model of the Atmosphere in the Infrared . 16 4.7 References . 24 5 Description of the Core Retrieval Algorithm Step I: Microwave Retrieval Algorithm 26 5.1 Introduction . 26 5.2 Precipitation Flags, Rate Retrieval and ATMS Corrections . 26 5.2.1 Precipitation Flags . 26 5.2.2 Perturbation Corrections . 27 5.2.3 Rain Rate Retrieval Algorithm . 27 5.3 Profile Retrieval Algorithm . 29 5.3.1 Preliminary Surface Type Classification . 29 5.3.2 Atmospheric Moisture and Condensation Model . 29 5.3.3 Estimation of surface brightness and atmospheric moisture . 30 5.3.4 iteration procedure and convergence tests . -
Laser Beacon Tracking for Free-Space Optical Communication
Laser Beacon Tracking for Free-space Optical Communication on Small-Satellite Platforms in Low-Earth Orbit by Tam Nguyen Thuc Nguyen S.B., Massachusetts Institute of Technology (2013) Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY September 2015 ○c Massachusetts Institute of Technology 2015. All rights reserved. Author................................................................ Department of Aeronautics and Astronautics August 20, 2015 Certified by. Kerri Cahoy Assistant Professor of Aeronautics and Astronautics Thesis Supervisor Accepted by........................................................... Paulo Lozano Chairman, Department Committee on Graduate Theses 2 Laser Beacon Tracking for Free-space Optical Communication on Small-Satellite Platforms in Low-Earth Orbit by Tam Nguyen Thuc Nguyen Submitted to the Department of Aeronautics and Astronautics on August 20, 2015, in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics Abstract Free-space optical (FSO) communication, or laser communication, is capable of pro- viding high-rate communication links, meeting the growing downlink demand of space missions, including those on small-satellite platforms. FSO communication takes ad- vantage of the high-gain nature of narrow laser beams to achieve higher link efficiency than traditional radio-frequency systems. In order for a FSO link to be established and maintained, the spacecraft’s attitude determination and control system needs to provide accurate pointing at the optical ground station. However, small satellites, such as CubeSats, have limited ground-tracking capabilities with existing attitude sen- sors. Miniaturized laser beacon tracking system, on the other hand, has the potential to provide precise ground-based attitude knowledge, enabling laser communication to be accomplished on small-satellite platforms. -
Annual Report of the Academic Year 2017-18 Sr
ANNUAL REPORT OF THE ACADEMIC YEAR 2017-18 SR. PAGE EVENT NAME NO. NO. 1. About DJSCE IETE 1 2. DJ SPARK 2017 2 3. Student Committee 6 4. IETE Fortnight 7 4.1 MATLAB Workshop 8 4.2 Arduino Workshop 9 4.3 Lecture on Power Electronics 10 4.4 Seminar on How To Write A Technical Paper 11 4.5 Seminar on How To Write A Resume 12 4.6 Ethical Hacking Workshop 13 4.7 PCB Designing Workshop 14 5. Artificial Intelligence and Computer Vision 15 Workshop 6. Lecture on Smith Charts 16 7. Technical Talk on Audio and Speech Processing 17 8. Technical Talk on Artificial Intelligence and 18 Network Securities 9. Industrial Visit to GMRT 19 10. DJ Strike 2017-18 20 11. ICWiCOM 2017 23 12. CANSAT 25 13. Website Launch 26 14. Blogs 27 15. Book Bank 28 16. Component Bank 29 17. DJ IGNITE 30 18. Interview Section 31 19. DJ SPARK 2018 32 ABOUT DJSCE IETE IETE (Institution of Electronics and Telecommunication Engineers) is a professional society for the advancement of scientific and technologically bent minds in the field of Electronics and Telecommunication. IETE consists of two streams of student base. First wing is the students of alma-mater, IETE, viz. the pass outs of DIPIETE, AMIETE and ALCCS students which forms an Alumni Association. The second wing is the Engineering students studying in Engineering Colleges and Polytechnics across the Country. This wing is the IETE-SF (IETE Students Forum). The IETE Student’s Forum of D.J. Sanghvi College of Engineering was founded in 2005. -
GOES-R Advanced Baseline Imager (ABI)
NOAA NESDIS CENTER for SATELLITE APPLICATIONS and RESEARCH GOES-R Advanced Baseline Imager (ABI) Algorithm Theoretical Basis Document For Legacy Atmospheric Moisture Profile, Legacy Atmospheric Temperature Profile, Total Precipitable Water, and Derived Atmospheric Stability Indices Jun Li, CIMSS/University of Wisconsin-Madison Timothy J. Schmit, STAR/NESDIS/NOAA Xin Jin, CIMSS/University of Wisconsin-Madison Graeme Martin, CIMSS/University of Wisconsin-Madison CIMSS sounding team Algorithm Integration Team Version 3.0 July 30, 2012 TABLE OF CONTENTS LIST OF FIGURES LIST OF TABLES LIST OF ACRONYMS ABSTRACT 1 INTRODUCTION ....................................................................................................... 12 1.1 Purpose of This Document ................................................................................... 12 1.2 Who Should Use This Document ......................................................................... 12 1.3 Inside Each Section .............................................................................................. 12 1.4 Related Documents ............................................................................................... 13 1.5 Revision History ................................................................................................... 13 2 OBSERVING SYSTEM OVERVIEW ....................................................................... 14 2.1 Products Generated ............................................................................................... 14 2.2 Instrument