Towards a Satellite System for Archaeology?
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Analysis of Perturbations and Station-Keeping Requirements in Highly-Inclined Geosynchronous Orbits
ANALYSIS OF PERTURBATIONS AND STATION-KEEPING REQUIREMENTS IN HIGHLY-INCLINED GEOSYNCHRONOUS ORBITS Elena Fantino(1), Roberto Flores(2), Alessio Di Salvo(3), and Marilena Di Carlo(4) (1)Space Studies Institute of Catalonia (IEEC), Polytechnic University of Catalonia (UPC), E.T.S.E.I.A.T., Colom 11, 08222 Terrassa (Spain), [email protected] (2)International Center for Numerical Methods in Engineering (CIMNE), Polytechnic University of Catalonia (UPC), Building C1, Campus Norte, UPC, Gran Capitan,´ s/n, 08034 Barcelona (Spain) (3)NEXT Ingegneria dei Sistemi S.p.A., Space Innovation System Unit, Via A. Noale 345/b, 00155 Roma (Italy), [email protected] (4)Department of Mechanical and Aerospace Engineering, University of Strathclyde, 75 Montrose Street, Glasgow G1 1XJ (United Kingdom), [email protected] Abstract: There is a demand for communications services at high latitudes that is not well served by conventional geostationary satellites. Alternatives using low-altitude orbits require too large constellations. Other options are the Molniya and Tundra families (critically-inclined, eccentric orbits with the apogee at high latitudes). In this work we have considered derivatives of the Tundra type with different inclinations and eccentricities. By means of a high-precision model of the terrestrial gravity field and the most relevant environmental perturbations, we have studied the evolution of these orbits during a period of two years. The effects of the different perturbations on the constellation ground track (which is more important for coverage than the orbital elements themselves) have been identified. We show that, in order to maintain the ground track unchanged, the most important parameters are the orbital period and the argument of the perigee. -
Astrodynamics
Politecnico di Torino SEEDS SpacE Exploration and Development Systems Astrodynamics II Edition 2006 - 07 - Ver. 2.0.1 Author: Guido Colasurdo Dipartimento di Energetica Teacher: Giulio Avanzini Dipartimento di Ingegneria Aeronautica e Spaziale e-mail: [email protected] Contents 1 Two–Body Orbital Mechanics 1 1.1 BirthofAstrodynamics: Kepler’sLaws. ......... 1 1.2 Newton’sLawsofMotion ............................ ... 2 1.3 Newton’s Law of Universal Gravitation . ......... 3 1.4 The n–BodyProblem ................................. 4 1.5 Equation of Motion in the Two-Body Problem . ....... 5 1.6 PotentialEnergy ................................. ... 6 1.7 ConstantsoftheMotion . .. .. .. .. .. .. .. .. .... 7 1.8 TrajectoryEquation .............................. .... 8 1.9 ConicSections ................................... 8 1.10 Relating Energy and Semi-major Axis . ........ 9 2 Two-Dimensional Analysis of Motion 11 2.1 ReferenceFrames................................. 11 2.2 Velocity and acceleration components . ......... 12 2.3 First-Order Scalar Equations of Motion . ......... 12 2.4 PerifocalReferenceFrame . ...... 13 2.5 FlightPathAngle ................................. 14 2.6 EllipticalOrbits................................ ..... 15 2.6.1 Geometry of an Elliptical Orbit . ..... 15 2.6.2 Period of an Elliptical Orbit . ..... 16 2.7 Time–of–Flight on the Elliptical Orbit . .......... 16 2.8 Extensiontohyperbolaandparabola. ........ 18 2.9 Circular and Escape Velocity, Hyperbolic Excess Speed . .............. 18 2.10 CosmicVelocities -
Evaluation of Stereoscopic Geoeye-1 Satellite Imagery to Assess Landscape and Stand Level Characteristics
EVALUATION OF STEREOSCOPIC GEOEYE-1 SATELLITE IMAGERY TO ASSESS LANDSCAPE AND STAND LEVEL CHARACTERISTICS K. Kliparchuk, M.Sc, GISP a, Dr. D. Collins, P.Geo. b a Hatfield Consultants Partnership, 200-850 Harbourside Drive, North Vancouver, BC, V7P0A3 Canada – [email protected] b BC Ministry of Forests and Range, Coast Forest Region, 2100 Labieux Road, Nanaimo, BC, V9T6E9, Canada - [email protected] Commission I, WG I/3 KEY WORDS: Remote sensing, GeoEye-1, effectiveness evaluation, forest resource management, stereo, photogrammetry ABSTRACT: An ongoing remote sensing project has been underway within the Coast Forest Region since 2000. The initial parts of the project investigated the application of commercially available high-resolution satellite imagery to resource feature mapping and compliance and enforcement surveillance. In the current project, stereo imagery from the new GeoEye-1 satellite was acquired. This system provides 0.5m panchromatic and 1.65m colour imagery, which is approximately a four time increase in spatial resolution compared to IKONOS imagery. Stereo imagery at this resolution enables the delineation of single trees, coarse woody debris measurement and the generation of Digital Elevation Models and estimation of volumes of material displaced by landslides. Change detection and identification of high priority zones for Compliance & Enforcement investigation is greatly enhanced. Results of this research are presented and discussed. 1. INTRODUCTION 1.1 Introduction The initial focus of the project was to investigate the application of commercially available high-resolution satellite imagery to resource feature mapping and compliance and enforcement surveillance. A previous published study by the authors in 2008 extended the use of high resolution IKONOS imagery through Figure 1. -
From Air, Sea, and Space, Geospatial Technology Is Helping Nations Monitor One of Their Biggest and Most Understated Threats: the Open Ocean
» CARDILLO AND LONG Q&A » FUTURE GEOINT LEADERS » SMALLSAT WORKING GROUP 2014 ISSUE 4 THE OFFICIAL MAGAZINE OF THE UNITED STATES GEOSPATIAL INTELLIGENCE FOUNDATION WATCHING THE 2014 USGIF MEMBERSHIP DIRECTORY WATERFrom air, sea, and space, geospatial technology is helping nations monitor one of their biggest and most understated threats: the open ocean. © DLR e.V. 2014 and © Airbus 2014 DS/© DLR Infoterra e.V. GmbH 2014 WorldDEMTM Reaching New Heights The new standard of global elevation models with pole-to-pole coverage, unrivalled accuracy and unique quality to support your critical missions. www.geo-airbusds.com/worlddem CONTENTS 2014 ISSUE 4 The USS Antietam (CG 54), the USS O’Kane (DDG 77) and the USS John C. Stennis (CVN 74) steam through the Gulf of Oman. As part of the John C. Stennis Carrier Strike Group, these ships are on regularly scheduled deployments in support of Maritime Operations, set- ting the conditions for security and stability, as well as complementing counterterrorism and security efforts to regional nations. PHOTO COURTESY OF U.S. NAVAL FORCES CENTRAL COMMAND/U.S. 5TH FLEET 5TH COMMAND/U.S. CENTRAL FORCES NAVAL U.S. OF COURTESY PHOTO 02 | VANTAGE POINT Features 12 | ELEVATE Tackling the challenge of Fayetteville State University accelerating innovation. builds GEOINT curriculum. 16 | WATCHING THE WATER From air, sea, and space, geospatial technology 14 | COMMON GROUND 04 | LETTERS is helping nations monitor one of their biggest USGIF stands up SmallSat Trajectory readers offer Working Group. feedback on recent features and most understated threats: the open ocean. and the tablet app. By Matt Alderton 32 | MEMBERSHIP PULSE Ball Aerospace offers 06 | INTSIDER 22 | CONVEYING CONSEQUENCE capabilities for an integrated SkyTruth and the GEOINT enterprise. -
Space Industry Paper 2008
Spring 2008 Industry Study Final Report Space Industry The Industrial College of the Armed Forces National Defense University Fort McNair, Washington, D.C. 20319-5062 i SPACE 2008 The United States space industry delivers capabilities vital to America’s economy, national security, and everyday life. America remains preeminent in the global space industry, but budget constraints, restrictive export policies, and limited international dialogue are inhibiting the U.S. space industry’s competitiveness. To sustain America’s leadership among space-faring nations, the incoming administration should update and expand U.S. space policies and regulatory guidance, prioritize national space funding, and promote greater international cooperation in space. These steps will strengthen U.S. space industry. They will also enhance U.S. national security, spur technological innovation, stimulate the national economy, and increase international cooperation and goodwill. Mr. Stephen M. Bloor, Dept of Defense Mr. Robert A. Burnes, Dept of the Navy CAPT John B. Carroll, US Navy CDR Charles J. Cassidy, US Navy COL Welton Chase, Jr., US Army CDR R. Duke Heinz, US Navy Lt Col Lawrence M. Hoffman, US Air Force COL Daniel R. Kestle, US Army LtCol Brian R. Kough, US Marine Corps Col Michael J. Miller, US Air Force CDR Albert G. Mousseau, US Navy CDR Robert D. Sharp, US Navy Mr. Howard S. Stronach, Federal Emergency Management Agency CDR L. Doug Stuffle, US Navy Mr. William J. Walls, Dept of State CAPT Kelly J. Wild, US Navy Dr. Scott A. Loomer, National Geospatial-Intelligence -
Maxar Technologies with Respect to Future Events, Financial Performance and Operational Capabilities
Leading Innovation in the New Space Economy Howard L. Lance President and Chief Executive Officer Forward-Looking Statement This presentation contains forward-looking statements and information, which reflect the current view of Maxar Technologies with respect to future events, financial performance and operational capabilities. The forward-looking statements in this presentation include statements as to managements’ expectations with respect to: the benefits of the transaction and strategic and integration opportunities; the company’s plans, objectives, expectations and intentions; expectations for sales growth, synergies, earnings and performance; shareholder value; and other statements that are not historical facts. Although management of the Company believes that the expectations and assumptions on which such forward-looking statements are based are reasonable, undue reliance should not be placed on the forward-looking statements because the Company can give no assurance that they will prove to be correct. Any such forward-looking statements are subject to various risks and uncertainties which could cause actual results and experience to differ materially from the anticipated results or expectations expressed in this presentation. Additional information concerning these risk factors can be found in the Company’s filings with Canadian securities regulatory authorities, which are available online under the Company’s profile at www.sedar.com, the Company’s filings with the United States Securities and Exchange Commission, or on the Company’s website at www.maxar.com, and in DigitalGlobe’s filings with the SEC, including Item 1A of DigitalGlobe’s Annual Report on Form 10-K for the year ended December 31, 2016. The forward-looking statements contained in this presentation are expressly qualified in their entirety by the foregoing cautionary statements and are based upon data available as of the date of this release and speak only as of such date. -
Aerospace, Defense, and Government Services Mergers & Acquisitions
Aerospace, Defense, and Government Services Mergers & Acquisitions (January 1993 - April 2020) Huntington BAE Spirit Booz Allen L3Harris Precision Rolls- Airbus Boeing CACI Perspecta General Dynamics GE Honeywell Leidos SAIC Leonardo Technologies Lockheed Martin Ingalls Northrop Grumman Castparts Safran Textron Thales Raytheon Technologies Systems Aerosystems Hamilton Industries Royce Airborne tactical DHPC Technologies L3Harris airport Kopter Group PFW Aerospace to Aviolinx Raytheon Unisys Federal Airport security Hydroid radio business to Hutchinson airborne tactical security businesses Vector Launch Otis & Carrier businesses BAE Systems Dynetics businesses to Leidos Controls & Data Premiair Aviation radios business Fiber Materials Maintenance to Shareholders Linndustries Services to Valsef United Raytheon MTM Robotics Next Century Leidos Health to Distributed Energy GERAC test lab and Technologies Inventory Locator Service to Shielding Specialities Jet Aviation Vienna PK AirFinance to ettain group Night Vision business Solutions business to TRC Base2 Solutions engineering to Sopemea 2 Alestis Aerospace to CAMP Systems International Hamble aerostructure to Elbit Systems Stormscope product eAircraft to Belcan 2 GDI Simulation to MBDA Deep3 Software Apollo and Athene Collins Psibernetix ElectroMechanical Aciturri Aeronautica business to Aernnova IMX Medical line to TransDigm J&L Fiber Services to 0 Knight Point Aerospace TruTrak Flight Systems ElectroMechanical Systems to Safran 0 Pristmatic Solutions Next Generation 911 to Management -
Geoeye Corp Overview
GeoEye See our World…Better than Ever 1 GeoEye Focus on Africa Ms. Andrea Cook Senior Sales Manager Middle East, Africa & India GeoEye GeoEye: Company Overview OfferingOffering bestbest resolutionresolution –– colorcolor –– accuracyaccuracy commerciallycommercially availableavailable 3 GeoEye: IKONOS and GeoEye-1 IKONOS – Launched 24 September 1999 – World’s first commercial satellite with 1- meter resolution • 0.82 meter panchromatic, 3.2 meters multi-spectral • Over 300 million km² of world-wide archive • Extensive global network of ground stations __________________________________________________________ GeoEye-1 – Launched 6 September 2008 – Started Commercial Operations 5 February 2009 – Most advanced satellite commercially available • 0.41 meter panchromatic, 1.65 multi- spectral • Designed for <5m accuracy without ground control • Up to 700,000 km² per day collection capacity (panchromatic) • >7 year mission life 4 IKONOS: 1 meter imagery AlmostAlmost 1010 yearsyears ofof archivearchive –– stillstill collectingcollecting strongstrong 5 GeoEye-1: First Images NowNow CommerciallyCommercially AvailableAvailable –– CollectingCollecting WorldWorld WideWide 6 GeoEye Constellation Collection Capacity Faster Response Times Faster Project Completions More Opportunities Served • GeoEye Constellation Collection Capacity – GeoEye-1 • Image 350,000 km2/day in multi-spectral mode • 700,000 sq km/day panchromatic mode – IKONOS • 150,000 sq km/day • True Constellation Operations for GeoEye-1 and IKONOS – Phased orbit Key: – Access to all locations -
Spectral Response for Digitalglobe Earth Imaging Instruments
Spectral Response for DigitalGlobe Earth Imaging Instruments IKONOS The IKONOS satellite carries a high resolution panchromatic band covering most of the silicon response and four lower resolution spectral bands. The four multispectral bands are roughly based on four bands used on the Landsat satellite series, including blue, green, red and near-infrared. The spectral responses of the bands are shown in Figure 1, individually normalized to the maximum value. Table 1 gives the 5% response upper and lower edges and center wavelengths for each. Figure1. Spectral Response of the IKONOS panchromatic and multispectral imagery. Table 1. IKONOS Spectral Band Edges and Center Wavelengths Band Name Center Lower Band Upper Band Edge Wavelength Edge (nm) (nm) (nm) Panchromatic 729 409 1048 Blue 480 421 539 Green 552 480 624 Red 666 602 729 NIR 803 713 893 2 QuickBird The QuickBird satellite also carries a high resolution panchromatic band covering most of the silicon response and four lower resolution spectral bands. The spectral responses of the bands are shown in Figure 2, individually normalized to the maximum value. Table 2 gives the 5% response upper and lower edges and center wavelengths for each. QuickBird Relative Spectral Radiance Response 1 0.9 0.8 0.7 Panchromatic Blue 0.6 Green Red NIR 0.5 0.4 Relative Response Relative 0.3 0.2 0.1 0 350 450 550 650 750 850 950 1050 Wavelength (nm) Figure 2. Spectral Response of the QuickBird panchromatic and multispectral imagery. Table 2. QuickBird Spectral Band Edges and Center Wavelengths Band Name Center Lower Band Upper Band Edge Wavelength Edge (nm) (nm) (nm) Panchromatic 729 405 1053 Blue 488 430 545 Green 543 466 620 Red 650 590 710 NIR 817 715 918 3 WorldView-1 The WorldView-1 satellite carries a panchromatic only instrument to produce basic black and white imagery for users who do not require color information. -
Small Satellites in Inclined Orbits to Increase Observation Capability Feasibility Analysis
International Journal of Pure and Applied Mathematics Volume 118 No. 17 2018, 273-287 ISSN: 1311-8080 (printed version); ISSN: 1314-3395 (on-line version) url: http://www.ijpam.eu Special Issue ijpam.eu Small Satellites in Inclined Orbits to Increase Observation Capability Feasibility Analysis DVA Raghava Murthy1, V Kesava Raju2, T.Ramanjappa3, Ritu Karidhal4, Vijayasree Mallikarjuna Kande5, G Ravi chandra Babu6 and A Arunachalam7 1 7 Earth Observations System, ISRO Headquarters, Bengaluru, Karnataka India [email protected] 2 4 5 6ISRO Satellite Centre, Bengaluru, Karnataka, India 3SK University, Ananthapur, Andhra Pradesh, India January 6, 2018 Abstract Over the period of past four decades, Remote Sensing data products and services have been effectively utilized to showcase varieties of applications in many areas of re- sources inventory and monitoring. There are several satel- lite systems in operation today and they operate from Po- lar Orbit and Geosynchronous Orbit, collect the imagery and non-imagery data and provide them to user community for various applications in the areas of natural resources management, urban planning and infrastructure develop- ment, weather forecasting and disaster management sup- port. Quality of information derived from Remote Sensing imagery are strongly influenced by spatial, spectral, radio- metric & temporal resolutions as well as by angular & po- larimetric signatures. As per the conventional approach of 1 273 International Journal of Pure and Applied Mathematics Special Issue having Remote Sensing satellites in near Polar Sun syn- chronous orbit, the temporal resolution, i.e. the frequency with which an area can be frequently observed, is basically defined by the swath of the sensor and distance between the paths. -
US National Security and Economic Interests in Remote Sensing
NATIONAL GEOSPATIAL-INTELLIGENCE AGENCY 7500 GEOINT Drive Springfield. Virginia 22150 Steven Aftergood Sent via U.S. mail Federation of American Scientists November 28,2012 1725 Desales Street NW, Suite 600 Re: FOIA Case Number: 20100025F Washington, DC 20036 Dear Mr. Aftergood: This letter responds to your October 29, 2009 Freedom oflnformation Act (FOIA) request, which we received on October 29, 2009. You requested access to documents pertaining to "U.S. National Security and Economic Interests in Remote Sensing: The Evolution of Civil and Commercial Policy by James A. Vedda, Aerospace Corp., February 20, 2009, preparedfor NGA Sensor Assimilation Division." , A search ofNGA's system of records located one document (37 pages) that is responsive to your request. We reviewed the responsive documents and determined they are releasable in full. If you have any questions about the way we handled your request, or about our FOIA regulations or procedures, please contact Elliott Bellinger, Deputy FOIA Program Manager, at 571-557-2994 or by email at [email protected] or via postal mail at: National Geospatial-Intelligence Agency FOIA Requester Service Center 7500 GEOINT Drive, MS S71-0GCA Springfield, VA 22150-7500 Sincerely, ~ Elliott Belinger Deputy FOIA Program Manager UNCLASSIFIED AEROSPACE REPORT NO. TOR-2009(3601 )-8539 U.S. National Security and Economic Interests in Remote Sensing: The Evolution of Civil and Commercial Policy 20 February 2009 James A. Yedda NSS Programs Policy and Oversight National Space Systems Engineering Prepared for: National Geospatial-Intelligence Agency Sensor Assimilation Division Sunrise Valley Drive Reston, VA 20191-3449 Contract No. FA8802-09-C-OOO 1 Authorized by: National Systems Group Distribution Statement: Distribution authorized to U.S. -
Open Rosen Thesis.Pdf
THE PENNSYLVANIA STATE UNIVERSITY SCHREYER HONORS COLLEGE DEPARTMENT OF AEROSPACE ENGINEERING END OF LIFE DISPOSAL OF SATELLITES IN HIGHLY ELLIPTICAL ORBITS MITCHELL ROSEN SPRING 2019 A thesis submitted in partial fulfillment of the requirements for a baccalaureate degree in Aerospace Engineering with honors in Aerospace Engineering Reviewed and approved* by the following: Dr. David Spencer Professor of Aerospace Engineering Thesis Supervisor Dr. Mark Maughmer Professor of Aerospace Engineering Honors Adviser * Signatures are on file in the Schreyer Honors College. i ABSTRACT Highly elliptical orbits allow for coverage of large parts of the Earth through a single satellite, simplifying communications in the globe’s northern reaches. These orbits are able to avoid drastic changes to the argument of periapse by using a critical inclination (63.4°) that cancels out the first level of the geopotential forces. However, this allows the next level of geopotential forces to take over, quickly de-orbiting satellites. Thus, a balance between the rate of change of the argument of periapse and the lifetime of the orbit is necessitated. This thesis sets out to find that balance. It is determined that an orbit with an inclination of 62.5° strikes that balance best. While this orbit is optimal off of the critical inclination, it is still near enough that to allow for potential use of inclination changes as a deorbiting method. Satellites are deorbited when the propellant remaining is enough to perform such a maneuver, and nothing more; therefore, the less change in velocity necessary for to deorbit, the better. Following the determination of an ideal highly elliptical orbit, the different methods of inclination change is tested against the usual method for deorbiting a satellite, an apoapse burn to lower the periapse, to find the most propellant- efficient method.