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Estimation of Gravity Wave Momentum Flux with Spectroscopic Imaging
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Embry-Riddle Aeronautical University Physical Sciences - Daytona Beach College of Arts & Sciences 1-2005 Estimation of Gravity Wave Momentum Flux with Spectroscopic Imaging Jing Tang Farzad Kamalabadi Steven J. Franke Alan Z. Liu Embry Riddle Aeronautical University - Daytona Beach, [email protected] Gary R. Swenson Follow this and additional works at: https://commons.erau.edu/db-physical-sciences Part of the Oceanography and Atmospheric Sciences and Meteorology Commons Scholarly Commons Citation Tang, J., Kamalabadi, F., Franke, S. J., Liu, A. Z., & Swenson, G. R. (2005). Estimation of Gravity Wave Momentum Flux with Spectroscopic Imaging. IEEE Transactions on Geoscience and Remote Sensing, 43(1). Retrieved from https://commons.erau.edu/db-physical-sciences/21 This Article is brought to you for free and open access by the College of Arts & Sciences at Scholarly Commons. It has been accepted for inclusion in Physical Sciences - Daytona Beach by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING, VOL. 43, NO. 1, JANUARY 2005 103 Estimation of Gravity Wave Momentum Flux With Spectroscopic Imaging Jing Tang, Student Member, IEEE, Farzad Kamalabadi, Member, IEEE, Steven J. Franke, Senior Member, IEEE, Alan Z. Liu, and Gary R. Swenson, Member, IEEE Abstract—Atmospheric gravity waves play a significant role waves is quantified by the divergence of the momentum flux. in the dynamics and thermal balance of the upper atmosphere. Using spectroscopic imaging to measure momentum flux will In this paper, we present a novel technique for automated contribute to the understanding of gravity wave processes and and robust calculation of momentum flux of high-frequency their influence on global circulation. -
Mars Express Orbiter Radio Science
MaRS: Mars Express Orbiter Radio Science M. Pätzold1, F.M. Neubauer1, L. Carone1, A. Hagermann1, C. Stanzel1, B. Häusler2, S. Remus2, J. Selle2, D. Hagl2, D.P. Hinson3, R.A. Simpson3, G.L. Tyler3, S.W. Asmar4, W.I. Axford5, T. Hagfors5, J.-P. Barriot6, J.-C. Cerisier7, T. Imamura8, K.-I. Oyama8, P. Janle9, G. Kirchengast10 & V. Dehant11 1Institut für Geophysik und Meteorologie, Universität zu Köln, D-50923 Köln, Germany Email: [email protected] 2Institut für Raumfahrttechnik, Universität der Bundeswehr München, D-85577 Neubiberg, Germany 3Space, Telecommunication and Radio Science Laboratory, Dept. of Electrical Engineering, Stanford University, Stanford, CA 95305, USA 4Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91009, USA 5Max-Planck-Instuitut für Aeronomie, D-37189 Katlenburg-Lindau, Germany 6Observatoire Midi Pyrenees, F-31401 Toulouse, France 7Centre d’etude des Environnements Terrestre et Planetaires (CETP), F-94107 Saint-Maur, France 8Institute of Space & Astronautical Science (ISAS), Sagamihara, Japan 9Institut für Geowissenschaften, Abteilung Geophysik, Universität zu Kiel, D-24118 Kiel, Germany 10Institut für Meteorologie und Geophysik, Karl-Franzens-Universität Graz, A-8010 Graz, Austria 11Observatoire Royal de Belgique, B-1180 Bruxelles, Belgium The Mars Express Orbiter Radio Science (MaRS) experiment will employ radio occultation to (i) sound the neutral martian atmosphere to derive vertical density, pressure and temperature profiles as functions of height to resolutions better than 100 m, (ii) sound -
Comparison Between GPS Radio Occultation and Radiosonde Sounding Data
Comparison Between GPS Radio Occultation and Radiosonde Sounding Data Dione Rossiter Academic Affiliation, Fall 2003: Senior University of California, Berkeley SOARS® Summer 2003 Science Research Mentors: Christian Rocken, Bill Kuo, and Bill Schreiner Writing and Communications Mentor: David Gochis Community Mentor: Annette Lampert Peer Mentor: Pauline Datulayta ABSTRACT Global Positioning System (GPS) Radio Occultation (RO) is a new technique for obtaining profiles of atmospheric properties, specifically: refractivity, temperature, pressure, water vapor pressure in the neutral atmosphere, and electron density in the ionosphere. The data received from GPS RO contribute significant amounts of information to a range of fields including meteorology, climate, ionospheric research, geodesy, and gravity. Low-Earth orbiting satellites, equipped with a GPS receiver, track GPS radio signals as they set or rise behind the Earth. Since GPS signals are refracted (delayed and bent) by the Earth's atmosphere, these data are used to infer information about atmospheric refractivity. Before the GPS RO data are used for research and operations, it is essential to assess their accuracy. Therefore, this research provided quantitative estimates of the accuracy of GPS RO when compared with measurements of known accuracy. Profile statistics (mean, standard deviation, standard error) were computed as a function of altitude to quantify the errors. Comparing RO data with nearby (300km; 2hr) radiosonde data yielded small mean error for all of the statistical plots generated, affirming that the RO technique is accurate for measuring atmospheric properties. Comparison of RO data with sounding data from different radiosonde systems showed that the RO technique was of high enough accuracy to differentiate differences in performance of various types of radiosonde systems. -
History of Frontal Concepts Tn Meteorology
HISTORY OF FRONTAL CONCEPTS TN METEOROLOGY: THE ACCEPTANCE OF THE NORWEGIAN THEORY by Gardner Perry III Submitted in Partial Fulfillment of the Requirements for the Degree of Bachelor of Science at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY June, 1961 Signature of'Author . ~ . ........ Department of Humangties, May 17, 1959 Certified by . v/ .-- '-- -T * ~ . ..... Thesis Supervisor Accepted by Chairman0 0 e 0 o mmite0 0 Chairman, Departmental Committee on Theses II ACKNOWLEDGMENTS The research for and the development of this thesis could not have been nearly as complete as it is without the assistance of innumerable persons; to any that I may have momentarily forgotten, my sincerest apologies. Conversations with Professors Giorgio de Santilw lana and Huston Smith provided many helpful and stimulat- ing thoughts. Professor Frederick Sanders injected thought pro- voking and clarifying comments at precisely the correct moments. This contribution has proven invaluable. The personnel of the following libraries were most cooperative with my many requests for assistance: Human- ities Library (M.I.T.), Science Library (M.I.T.), Engineer- ing Library (M.I.T.), Gordon MacKay Library (Harvard), and the Weather Bureau Library (Suitland, Md.). Also, the American Meteorological Society and Mr. David Ludlum were helpful in suggesting sources of material. In getting through the myriad of minor technical details Professor Roy Lamson and Mrs. Blender were indis-. pensable. And finally, whatever typing that I could not find time to do my wife, Mary, has willingly done. ABSTRACT The frontal concept, as developed by the Norwegian Meteorologists, is the foundation of modern synoptic mete- orology. The Norwegian theory, when presented, was rapidly accepted by the world's meteorologists, even though its several precursors had been rejected or Ignored. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
2018: Aiaa-Space-Report
AIAA TEAM SPACE TRANSPORTATION DESIGN COMPETITION TEAM PERSEPHONE Submitted By: Chelsea Dalton Ashley Miller Ryan Decker Sahil Pathan Layne Droppers Joshua Prentice Zach Harmon Andrew Townsend Nicholas Malone Nicholas Wijaya Iowa State University Department of Aerospace Engineering May 10, 2018 TEAM PERSEPHONE Page I Iowa State University: Persephone Design Team Chelsea Dalton Ryan Decker Layne Droppers Zachary Harmon Trajectory & Propulsion Communications & Power Team Lead Thermal Systems AIAA ID #908154 AIAA ID #906791 AIAA ID #532184 AIAA ID #921129 Nicholas Malone Ashley Miller Sahil Pathan Joshua Prentice Orbit Design Science Science Science AIAA ID #921128 AIAA ID #922108 AIAA ID #761247 AIAA ID #922104 Andrew Townsend Nicholas Wijaya Structures & CAD Trajectory & Propulsion AIAA ID #820259 AIAA ID #644893 TEAM PERSEPHONE Page II Contents 1 Introduction & Problem Background2 1.1 Motivation & Background......................................2 1.2 Mission Definition..........................................3 2 Mission Overview 5 2.1 Trade Study Tools..........................................5 2.2 Mission Architecture.........................................6 2.3 Planetary Protection.........................................6 3 Science 8 3.1 Observations of Interest.......................................8 3.2 Goals.................................................9 3.3 Instrumentation............................................ 10 3.3.1 Visible and Infrared Imaging|Ralph............................ 11 3.3.2 Radio Science Subsystem................................. -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center
DSCOVR Magnetometer Observations Adam Szabo, Andriy Koval NASA Goddard Space Flight Center 1 Locations of the Instruments Faraday Cup EPIC Omni Antenna Star Tracker Thruster Modules Digital Sun Sensor Electron Spectrometer +Z +X Magnetometer +Y 2 Goddard Fluxgate Magnetometer The Fluxgate Magnetometer measures the interplanetary vector magnetic field It is located at the tip of a 4.0 m boom to minimize the effect of spacecraft fields Requirement Value Method Performance Magnetometer Range 0.1-100 nT Test 0.004-65,500 nT Accuracy +/- 1 nT Measured +/- 0.2 nT Cadence 1 min Measured 50 vector/sec 3 Pre-flight Calibration • Determined the magnetometer zero levels, scale factors, and magnetometer orthogonalization matrix. • Determined the spacecraft generated magnetic fields – Subsystem level magnetic tests. Reaction wheels, major source of dynamic field, were shielded – Spacecraft unpowered magnetic test in the GSFC 40’ magnetic facility In-Flight Boom Deployment • Nominal deployment on 2/15/15, seen as 4.4 rotations in the magnetometer components Mostly spacecraft Boom deployment Interplanetary magnetic field induced fields 5 Alfven Waves in the Solar Wind • The solar wind contains magnetic field rotations that preserve the magnitude of the field, so called Alfven waves. • Alfven waves are ubiquitous and are possible to identify with automated routines. • Systematic deviations from a constant field magnitude during these waves are an indication of spacecraft induced offsets. • Minimizing the deviations with slowly changing offsets allows in-flight calibrations. 6 In-Flight Magnetometer Calibrations Z Magnetometer Zero Offsets X • X axis Roll and Z axis Slew data is Y consistent with ground calibration estimates X • Independent zero offset determination by rolls, slews and using solar wind Alfvenicity give consistent values Z • Time variation is consistent with yearly orbital change. -
Accessing Pds Data in Pipeline Processing and Web Sites Through Pds Geosciences Orbital Data Explorer’S Web-Based Api (Rest) Interface
45th Lunar and Planetary Science Conference (2014) 1026.pdf ACCESSING PDS DATA IN PIPELINE PROCESSING AND WEB SITES THROUGH PDS GEOSCIENCES ORBITAL DATA EXPLORER’S WEB-BASED API (REST) INTERFACE. K. J. Bennett, J. Wang, D. Scholes, Washington University in St. Louis, 1 Brookings Drive, Campus Box 1169, St. Louis, Missouri, 63130, {bennett, wang, sholes}@wunder.wustl.edu. Introduction: The Orbital Data Explorer (ODE) is tem (RSS). a web-based search tool (http://ode.rsl.wustl.edu) de- High Resolution Stereo Camera (HRSC), Mars Advanced Radar for Subsurface and Iono- veloped at NASA’s Planetary Data System’s (PDS) sphere Sounding (MARSIS), OMEGA Geosciences Node (http://pds-geosciences.wustl.edu/). Mars Express (Observatoire Mineralogie, Eau, Glaces, Through ODE, users can search, browse, and download Activite) Visible and Infrared Mineralogical a wide range of PDS Mars, Moon, Mercury, and Venus Mapping Spectrometer, and Planetary Fourier Spectrometer (PFS). data ([1,2,3,4]). Mars Orbiter Laser Altimeter (MOLA), and Mars Global In the fall of 2012, the Geosciences node intro- MOC Narrow Angle (NA) and Wide Angle Surveyor (MGS) duced a simple web-based API that allows non-PDS (WA) cameras. Gamma Ray Spectrometer (GRS) and Thermal web and processing tools to search for PDS products, Odyssey Emission Imaging System (THEMIS) obtain meta-data about those products, and download Viking Orbiter Visual Imaging Subsystem Camera A/B the products stored in ODE’s meta-data database. The Gamma Ray Spectrometer (GRS), Radio Sci- first version is now used by several teams in periodic MESSENGER ence Subsystem (RSS), Neutron Spectrometer processing and web sites. -
An Approach to Magnetic Cleanliness for the Psyche Mission M
An Approach to Magnetic Cleanliness for the Psyche Mission M. de Soria-Santacruz J. Ream K. Ascrizzi ([email protected]), ([email protected]), ([email protected]) M. Soriano R. Oran University of Michigan Ann Arbor ([email protected]), ([email protected]), 500 S State St O. Quintero B. P. Weiss Ann Arbor, MI 48109 ([email protected]), ([email protected]) F. Wong Department of Earth, Atmospheric, ([email protected]), and Planetary Sciences S. Hart Massachusetts Institute of Technology ([email protected]), 77 Massachusetts Avenue M. Kokorowski Cambridge, MA 02139 ([email protected]) B. Bone ([email protected]), B. Solish ([email protected]), D. Trofimov ([email protected]), E. Bradford ([email protected]), C. Raymond ([email protected]), P. Narvaez ([email protected]) Jet Propulsion Laboratory, California Institute of Technology 4800 Oak Grove Drive Pasadena, CA 91109 C. Keys C. Russell L. Elkins-Tanton ([email protected]), ([email protected]), ([email protected]) P. Lord University of California Los Angeles Arizona State University ([email protected]) 405 Hilgard Avenue PO Box 871404 Maxar Technologies Inc. Los Angeles, CA 90095 Tempe, AZ 85287 3825 Fabian Avenue Palo Alto, CA 94303 Abstract— Psyche is a Discovery mission that will visit the fields. Limiting and characterizing spacecraft-generated asteroid (16) Psyche to determine if it is the metallic core of a magnetic fields is therefore essential to the mission. This is the once larger differentiated body or otherwise was formed from objective of the Psyche’s magnetics control program described accretion of unmelted metal-rich material. -
Abstracts of the 50Th DDA Meeting (Boulder, CO)
Abstracts of the 50th DDA Meeting (Boulder, CO) American Astronomical Society June, 2019 100 — Dynamics on Asteroids break-up event around a Lagrange point. 100.01 — Simulations of a Synthetic Eurybates 100.02 — High-Fidelity Testing of Binary Asteroid Collisional Family Formation with Applications to 1999 KW4 Timothy Holt1; David Nesvorny2; Jonathan Horner1; Alex B. Davis1; Daniel Scheeres1 Rachel King1; Brad Carter1; Leigh Brookshaw1 1 Aerospace Engineering Sciences, University of Colorado Boulder 1 Centre for Astrophysics, University of Southern Queensland (Boulder, Colorado, United States) (Longmont, Colorado, United States) 2 Southwest Research Institute (Boulder, Connecticut, United The commonly accepted formation process for asym- States) metric binary asteroids is the spin up and eventual fission of rubble pile asteroids as proposed by Walsh, Of the six recognized collisional families in the Jo- Richardson and Michel (Walsh et al., Nature 2008) vian Trojan swarms, the Eurybates family is the and Scheeres (Scheeres, Icarus 2007). In this theory largest, with over 200 recognized members. Located a rubble pile asteroid is spun up by YORP until it around the Jovian L4 Lagrange point, librations of reaches a critical spin rate and experiences a mass the members make this family an interesting study shedding event forming a close, low-eccentricity in orbital dynamics. The Jovian Trojans are thought satellite. Further work by Jacobson and Scheeres to have been captured during an early period of in- used a planar, two-ellipsoid model to analyze the stability in the Solar system. The parent body of the evolutionary pathways of such a formation event family, 3548 Eurybates is one of the targets for the from the moment the bodies initially fission (Jacob- LUCY spacecraft, and our work will provide a dy- son and Scheeres, Icarus 2011). -
Spire's Cubesat Constellation of GNSS, AIS, and ADS-B Sensors
Seizing Opportunity: Spire’s CubeSat Constellation of GNSS, AIS, and ADS-B Sensors Dallas Masters, Director of GNSS, Spire Global, Inc. Stanford PNT Symposium, 2018-11-08 WHO & WHAT IS SPIRE? We’re a new, innovative satellite & data services company that you might not have heard of… We’re what you get when you mix agile development with nanosatellites... We’re the transformation of a single , crowd-sourced nanosatellite into one of the largest constellations of satellites in the world... Stanford PNT Symposium, 2018-11-08 OUTLINE 1. Overview of Spire 2. Spire satellites and PNT payloads & products a. AIS ship tracking b. GNSS-based remote sensing measurements: radio occultation (RO), ionosphere electron density, bistatic radar (reflections) c. ADS-B aircraft tracking (early results) 3. Spire’s lofty long-term goals Stanford PNT Symposium, 2018-11-08 AN OVERVIEW OF SPIRE Stanford PNT Symposium, 2018-11-08 SPIRE TODAY • 150 people across five offices (a distributed start-up) - San Francisco, Boulder, Glasgow, Luxembourg, and Singapore • 60+ LEO 3U CubeSats (10x10x30 cm) in orbit with passive sensing payloads, 30+ global ground stations - 16 launch campaigns completed with seven different launch providers - Ground station network owned and operated in-house for highest level of security and resilience • Observing each point on Earth 100 times per day, everyday - Complete global coverage, including the polar regions • Deploying new applications within 6-12 month timeframes • World’s largest ship tracking constellation • World’s largest weather