Satellite Telemetry: a New Tool for Wildlife Research and Management
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TRACKING and DATA ACQUISITION/ SPACE OPERATIONS **DB Chap 4(297-321) 1/17/02 12:29 PM Page 299
**DB Chap 4(297-321) 1/17/02 12:29 PM Page 297 CHAPTER FOUR TRACKING AND DATA ACQUISITION/ SPACE OPERATIONS **DB Chap 4(297-321) 1/17/02 12:29 PM Page 299 CHAPTER FOUR TRACKING AND DATA ACQUISITION/ SPACE OPERATIONS Introduction NASA’s tracking and data acquisition program provided vital support for all NASA flight projects. NASA also supported, on a reimbursable basis, projects of the Department of Defense, other government agencies, commercial firms, and other countries and international organizations engaged in space research activities. The tracking and data acquisition program supported sounding rock- ets and balloons, research aircraft, Earth orbital and suborbital missions, planetary spacecraft, and deep space probes. The support included: • Tracking to determine the position and trajectory of vehicles in space • Acquisition of scientific and Earth applications data from on-board experiments and sensors • Acquisition of engineering data on the performance of spacecraft and launch vehicle systems • Transmission of commands from ground stations to spacecraft • Communication with astronauts • Communication of information among the various ground facilities and central control centers • Processing of data acquired from launch vehicles and spacecraft • Reception of television transmission from space vehicles NASA established three types of support capabilities: • The Spaceflight Tracking and Data Network (STDN) supported low- Earth orbital missions. • The Deep Space Network (DSN) supported planetary and interplane- tary flight missions. It also supported geosynchronous and highly elliptical missions and those in low-Earth orbit not compatible with the Tracking and Data Relay Satellite System (TDRSS). • The TDRSS provided low-Earth orbital mission support and reduced NASA’s need for an extensive network of ground stations. -
25 Years of Indian Remote Sensing Satellite (IRS)
2525 YearsYears ofof IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) SeriesSeries Vinay K Dadhwal Director National Remote Sensing Centre (NRSC), ISRO Hyderabad, INDIA 50 th Session of Scientific & Technical Subcommittee of COPUOS, 11-22 Feb., 2013, Vienna The Beginning • 1962 : Indian National Committee on Space Research (INCOSPAR), at PRL, Ahmedabad • 1963 : First Sounding Rocket launch from Thumba (Nov 21, 1963) • 1967 : Experimental Satellite Communication Earth Station (ESCES) established at Ahmedabad • 1969 : Indian Space Research Organisation (ISRO) established (15 August) PrePre IRSIRS --1A1A SatellitesSatellites • ARYABHATTA, first Indian satellite launched in April 1975 • Ten satellites before IRS-1A (7 for EO; 2 Met) • 5 Procured & 5 SLV / ASLV launch SAMIR : 3 band MW Radiometer SROSS : Stretched Rohini Series Satellite IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) –– 1A1A • First Operational EO Application satellite, built in India, launch USSR • Carried 4-band multispectral camera (3 nos), 72m & 36m resolution Satellite Launch: March 17, 1988 Baikanur Cosmodrome Kazakhstan SinceSince IRSIRS --1A1A • Established of operational EO activities for – EO data acquisition, processing & archival – Applications & institutionalization – Public services in resource & disaster management – PSLV Launch Program to support EO missions – International partnership, cooperation & global data sets EarlyEarly IRSIRS MultispectralMultispectral SensorsSensors • 1st Generation : IRS-1A, IRS-1B • -
The Space-Based Global Observing System in 2010 (GOS-2010)
WMO Space Programme SP-7 The Space-based Global Observing For more information, please contact: System in 2010 (GOS-2010) World Meteorological Organization 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int WMO Space Programme Office Tel.: +41 (0) 22 730 85 19 – Fax: +41 (0) 22 730 84 74 E-mail: [email protected] Website: www.wmo.int/pages/prog/sat/ WMO-TD No. 1513 WMO Space Programme SP-7 The Space-based Global Observing System in 2010 (GOS-2010) WMO/TD-No. 1513 2010 © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0)22 730 84 03 P.O. Box No. 2300 Fax: +41 (0)22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] FOREWORD The launching of the world's first artificial satellite on 4 October 1957 ushered a new era of unprecedented scientific and technological achievements. And it was indeed a fortunate coincidence that the ninth session of the WMO Executive Committee – known today as the WMO Executive Council (EC) – was in progress precisely at this moment, for the EC members were very quick to realize that satellite technology held the promise to expand the volume of meteorological data and to fill the notable gaps where land-based observations were not readily available. -
Accuracy, Precision, and Performance of Satellite Telemetry for Monitoring Wolf Movements Within Each Category
Accuracy, Precision, and Pedormance of Satellite Telemetry for Monitoring Wolf Movements • Warren B. Ballard, Daniel J. Reed, Steven G. Fancy, and Paul R. Krausman We placed 23 satellite platform transmitter terminals (1.08-I.22 kg) on wolves in northwest Alaska during I987 through I99I. Male and female wolves aged I 0 months to eight years were monitored with no apparent adverse effects on them. We obtained 3 ,80I relocations from the 23 transmitters, an average of 29 relocations/month from each. Transmitters were programmed to operate four to six hours every two days and had a mean life span (including days before and after use on a wolf) of253 days (range= 67-482 days). Average life span while attached to wolves was I8I days (range= 50-366 days). Accuracy of I ,885 relocations at seven known sites varied among transmitters and averaged 336 and 728 mfor best and low quality relocations, respectively. The estimated locations from several transmitters were biased toward south and west directions. Costs (I992) per satellite relocation averaged about $44 U.S., in comparison to about $I66 with conventional telemetry methods using fixed-wing aircraft. Satellite telemetry has great potential for providing improved data sets for evaluation ofwolfterritory sizes and movements, but currently lacks accuracy and precision for detailed habitat or landscape use assessments. Introduction three reports provided evaluations of the systems after 1987 when Service Argos made improvements in calculating lo Satellite telemetry has become a widely accepted tool for cations and quality indices (Keating et al. 1991). Ofthe latter studying movements oflarge mammals and birds (Fancy et three studies, only Keating et al. -
Design of the Wavefront Sensor Unit of ARGOS, the LBT Laser Guide Star System
UNIVERSITA` DEGLI STUDI DI FIRENZE Dipartimento di Fisica e Astronomia Scuola di Dottorato in Astronomia Ciclo XXIV - FIS05 Design of the wavefront sensor unit of ARGOS, the LBT laser guide star system Candidato: Marco Bonaglia arXiv:1203.5081v1 [astro-ph.IM] 22 Mar 2012 Tutore: Prof. Alberto Righini Cotutore: Dott. Simone Esposito A common use for a glass plate is as a beam splitter, tilted at an angle of 45◦ [:::] Since this can severely degrade the image, such plate beam splitters are not recommended in convergent or divergent beams. W. J. Smith, Modern Optical Engineering. Contents 1 Introduction 1 1.1 The Large Binocular Telescope . 2 1.2 LUCI . 4 1.3 First Light AO system . 5 1.3.1 Angular anisoplanatism . 8 1.4 Wide field AO correction . 9 1.5 Laser guide star AO . 10 1.5.1 Limits of LGS AO . 11 1.5.2 Rayleigh LGS . 13 1.6 LGS-GLAO facilities . 14 1.6.1 GLAS . 15 1.6.2 The MMT GLAO system . 15 1.6.3 SAM . 18 2 ARGOS: a laser guide star AO system for the LBT 21 2.1 System design . 22 2.2 Study of ARGOS performance . 29 2.2.1 The simulation code . 30 2.2.2 Results of ARGOS end-to-end simulations . 36 3 The wavefront sensor dichroic 43 3.1 Effects of a window in a convergent beam . 43 3.2 Aberration compensation with window shape . 47 3.2.1 Effects of a wedge between surfaces . 48 3.2.2 Effects of a cylindrical surface . -
The Rings and Inner Moons of Uranus and Neptune: Recent Advances and Open Questions
Workshop on the Study of the Ice Giant Planets (2014) 2031.pdf THE RINGS AND INNER MOONS OF URANUS AND NEPTUNE: RECENT ADVANCES AND OPEN QUESTIONS. Mark R. Showalter1, 1SETI Institute (189 Bernardo Avenue, Mountain View, CA 94043, mshowal- [email protected]! ). The legacy of the Voyager mission still dominates patterns or “modes” seem to require ongoing perturba- our knowledge of the Uranus and Neptune ring-moon tions. It has long been hypothesized that numerous systems. That legacy includes the first clear images of small, unseen ring-moons are responsible, just as the nine narrow, dense Uranian rings and of the ring- Ophelia and Cordelia “shepherd” ring ε. However, arcs of Neptune. Voyager’s cameras also first revealed none of the missing moons were seen by Voyager, sug- eleven small, inner moons at Uranus and six at Nep- gesting that they must be quite small. Furthermore, the tune. The interplay between these rings and moons absence of moons in most of the gaps of Saturn’s rings, continues to raise fundamental dynamical questions; after a decade-long search by Cassini’s cameras, sug- each moon and each ring contributes a piece of the gests that confinement mechanisms other than shep- story of how these systems formed and evolved. herding might be viable. However, the details of these Nevertheless, Earth-based observations have pro- processes are unknown. vided and continue to provide invaluable new insights The outermost µ ring of Uranus shares its orbit into the behavior of these systems. Our most detailed with the tiny moon Mab. Keck and Hubble images knowledge of the rings’ geometry has come from spanning the visual and near-infrared reveal that this Earth-based stellar occultations; one fortuitous stellar ring is distinctly blue, unlike any other ring in the solar alignment revealed the moon Larissa well before Voy- system except one—Saturn’s E ring. -
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). -
+ Return to Flight Implementation Plan -- 12Th Edition (8.4 Mb PDF)
NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond A periodically updated document demonstrating our progress toward safe return to flight and implementation of the Columbia Accident Investigation Board recommendations June 20, 2006 Volume 1, Twelfth Edition An electronic version of this implementation plan is available at www.nasa.gov NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond June 20, 2006 Twelfth Edition Change June 20, 2006 This 12th revision to NASA’s Implementation Plan for Space Shuttle Return to Flight and Beyond provides updates to three Columbia Accident Investigation Board Recommendations that were not fully closed by the Return to Flight Task Group, R3.2-1 External Tank (ET), R6.4-1 Thermal Protection System (TPS) On-Orbit Inspection and Repair, and R3.3-2 Orbiter Hardening and TPS Impact Tolerance. These updates reflect the latest status of work being done in preparation for the STS-121 mission. Following is a list of sections updated by this revision: Message from Dr. Michael Griffin Message from Mr. William Gerstenmaier Part 1 – NASA’s Response to the Columbia Accident Investigation Board’s Recommendations 3.2-1 External Tank Thermal Protection System Modifications (RTF) 3.3-2 Orbiter Hardening (RTF) 6.4-1 Thermal Protection System On-Orbit Inspect and Repair (RTF) Remove Pages Replace with Pages Cover (Feb 17, 2006) Cover (Jun. 20, 2006 ) Title page (Feb 17, 2006) Title page (Jun. 20, 2006) Message From Michael D. Griffin Message From Michael D. Griffin (Feb 17, 2006) -
Radio Telemetry and Bird Movements
95 Chapter 7 Radio telemetry and bird movements RADIO TELEMETRY Understanding the role that wildlife play in the ecology of AI viruses requires knowledge of the detailed movements of wild birds over varying spatial scales. On the one hand, con- currence between the migratory patterns of some Palearctic breeding waterbirds and the spread of the H5N1 HPAI virus across Asia and Europe in the northern fall and winter of 2005/06 illustrates the importance of studies designed to identify specific migratory routes, stopover points and non-breeding areas that may span entire continents. On the other hand, studies documenting the local movements of wild birds between poultry farms and nearby wetlands may be invaluable to establish viable pathways of H5N1 HPAI transmission from poultry to wildlife (or vice versa). Radio telemetry is a technique for determining bird movements over areas ranging in size from the restricted breeding territories of resident bird species to the movement pat- terns of international migratory species (reviewed in Fuller et al. 2005). Radio telemetry has important applications in the investigation of infectious diseases of migratory species, including H5N1 AI virus ecology. Specific objectives for AI-related telemetry studies have already been identified during the FAO-OIE International Scientific Conference on Avian Influenza and Wild Birds in May 200610. In fact, telemetry projects tracking the local move- ments and migration routes of wild birds identified as potential virus hosts are already under way11. The basic concept of a radio telemetry study sounds simple; attach a radio transmitter to an animal and track the signal to determine the animal’s movements. -
Demonstration of Satellite/GPS Telemetry for Monitoring Fine- Scale Movements of Lesser Prairie-Chickens
United States Department of Agriculture Forest Service National Technology & Demonstration of Development Program Inventory and Monitoring 1219 1813—SDTDC Satellite/GPS Telemetry December 2012 for Monitoring Fine- Scale Movements of Lesser Prairie-Chickens Demonstration of Satellite/GPS Telemetry for Monitoring Fine-Scale Movements of Lesser Prairie-Chickens Rey Farve, Project Leader Forest Service San Dimas Technology & Development Center December 2012 The information contained in this publication has been developed for the guidance of employees of the Forest Service, U.S. Department of Agriculture, its contractors, and cooperating Federal and State agencies. The Forest Service assumes no responsibility for the interpretation or use of this information by other than its own employees. The use of trade, firm, or corporation names is for the information and convenience of the reader. Such use does not constitute an official evaluation, conclusion, recommendation, endorsement, or approval of any product or service to the exclusion of others that may be suitable. The U.S. Department of Agriculture (USDA) prohibits discrimination in all its programs and activities on the basis of race, color, national origin, age, disability, and where applicable, sex, marital status, familial status, parental status, religion, sexual orientation, genetic information, political beliefs, reprisal, or because all or part of an individual’s income is derived from any public assistance program. (Not all prohibited bases apply to all programs.) Persons with disabilities who require alternative means for communication of program information (Braille, large print, audiotape, etc.) should contact USDA’s TARGET Center at (202) 720-2600 (voice and TDD). To file a complaint of discrimination, write USDA, Director, Office of Civil Rights, 1400 Independence Avenue, S.W., Washington, D.C. -
NASA Finds Neptune Moons Locked in 'Dance of Avoidance' 15 November 2019, by Gretchen Mccartney
NASA finds Neptune moons locked in 'dance of avoidance' 15 November 2019, by Gretchen McCartney Although the dance may appear odd, it keeps the orbits stable, researchers said. "We refer to this repeating pattern as a resonance," said Marina Brozovi?, an expert in solar system dynamics at NASA's Jet Propulsion Laboratory in Pasadena, California, and the lead author of the new paper, which was published Nov. 13 in Icarus. "There are many different types of 'dances' that planets, moons and asteroids can follow, but this one has never been seen before." Far from the pull of the Sun, the giant planets of the Neptune Moon Dance: This animation illustrates how the outer solar system are the dominant sources of odd orbits of Neptune's inner moons Naiad and gravity, and collectively, they boast dozens upon Thalassa enable them to avoid each other as they race dozens of moons. Some of those moons formed around the planet. Credit: NASA alongside their planets and never went anywhere; others were captured later, then locked into orbits dictated by their planets. Some orbit in the opposite direction their planets rotate; others swap orbits Even by the wild standards of the outer solar with each other as if to avoid collision. system, the strange orbits that carry Neptune's two innermost moons are unprecedented, according to Neptune has 14 confirmed moons. Neso, the newly published research. farthest-flung of them, orbits in a wildly elliptical loop that carries it nearly 46 million miles (74 million Orbital dynamics experts are calling it a "dance of kilometers) away from the planet and takes 27 avoidance" performed by the tiny moons Naiad years to complete. -
Filipiak Solar System Book
Our Solar System Mrs. Filipiak’s Class Our Solar System Mrs. Filipiak’s Class Sun ...............................................................................................7 Michael ........................................................................................7 Mercury ........................................................................................1 Denzel ..........................................................................................1 Mercury ........................................................................................3 Austin ...........................................................................................3 Mercury ........................................................................................5 Madison B ....................................................................................5 Venus ............................................................................................7 Shyla .............................................................................................7 Venus ............................................................................................9 Kenny ...........................................................................................9 Earth ..........................................................................................11 Kaleb ..........................................................................................11 Earth ..........................................................................................13