Application of On-board Micro-accelerometers for Orbit Determination of Space-VLBI Satellites

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (27 download)

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Book Synopsis Application of On-board Micro-accelerometers for Orbit Determination of Space-VLBI Satellites by : Ivan Almor

Download or read book Application of On-board Micro-accelerometers for Orbit Determination of Space-VLBI Satellites written by Ivan Almor and published by . This book was released on 1989 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites by : Frank A. Marcos

Download or read book Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites written by Frank A. Marcos and published by . This book was released on 1977 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive amount of neutral density data has been obtained from the highly successful accelerometer experiments on the Atmosphere Explorer -C, -D, and -E satellites. The accelerometer is electrostatically suspended and force rebalanced. Ground calibration requires sufficient suspension force to operate in the earth's 1g field. An important characteristic of the instrument is its null bias which is proportional to the suspension voltage. Null bias error is reduced when the instrument is in orbit by reducing the suspension force. For despun orbit data, accelerations due to bias must be separated from those due to drag for accurate density computation. In the elliptical orbit phase of the AE missions, bias values have been deduced from the sensor output obtained at altitudes where aerodynamic drag is negligible. Bias measurements obtained from all three satellites are summarized. A bias temperature coefficient is also calculated. Results in this report show that orbital values differ from a simple extrapolation of the ground calibration data. This difference must be known to obtain accurate density data above about 200 km. The orbital bias results are applied to improve the accuracy of despun orbit measurements made during both the elliptical and circular orbit phases of the AE mission. Methods of extending bias determination to circular orbit data are discussed. (Author).

Methods of Orbit Determination for the Microcomputer

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Publisher : Willmann-Bell
ISBN 13 :
Total Pages : 592 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Methods of Orbit Determination for the Microcomputer by : Dan L. Boulet

Download or read book Methods of Orbit Determination for the Microcomputer written by Dan L. Boulet and published by Willmann-Bell. This book was released on 1991 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of the Satellite Triaxial Accelerometer Experiment to Atmospheric Density and Wind Studies

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Application of the Satellite Triaxial Accelerometer Experiment to Atmospheric Density and Wind Studies by : Frank A. Marcos

Download or read book Application of the Satellite Triaxial Accelerometer Experiment to Atmospheric Density and Wind Studies written by Frank A. Marcos and published by . This book was released on 1982 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new satellite triaxial accelerometer system has been developed. This instrument has been flight-tested on three-axis stabilized satellites and has demonstrated the capability to accurately measure accelerations in the satellite's in-track, cross-track, and radial directions. The in-track data provide direct determination of atmospheric density. These data, obtained during a period of high solar flux, supplement the extensive set of measurements obtained by other accelerometer experiments during low solar flux conditions. The cross-track and radial results permit, for the first time, large-scale measurements of the zonal and, possibly, radial components of neutral atmospheric winds. These simultaneous wind and density data provide an extremely valuable input for the understanding of dynamic processes in the atmosphere and for the improvement of atmospheric models.

IEEE PLANS '92 Position Location and Navigation Symposium Record

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Publisher : Institute of Electrical & Electronics Engineers(IEEE)
ISBN 13 :
Total Pages : 586 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis IEEE PLANS '92 Position Location and Navigation Symposium Record by :

Download or read book IEEE PLANS '92 Position Location and Navigation Symposium Record written by and published by Institute of Electrical & Electronics Engineers(IEEE). This book was released on 1992 with total page 586 pages. Available in PDF, EPUB and Kindle. Book excerpt:

IEEE PLANS ...

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ISBN 13 :
Total Pages : 588 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis IEEE PLANS ... by :

Download or read book IEEE PLANS ... written by and published by . This book was released on 1992 with total page 588 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (17 download)

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Book Synopsis Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites by : Frank A. Marcos

Download or read book Orbital Bias Determination for Accelerometers on Atmosphere Explorer Satellites written by Frank A. Marcos and published by . This book was released on 1977 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive amount of neutral density data has been obtained from the highly successful accelerometer experiments on the Atmosphere Explorer -C, -D, and -E satellites. The accelerometer is electrostatically suspended and force rebalanced. Ground calibration requires sufficient suspension force to operate in the earth's 1g field. An important characteristic of the instrument is its null bias which is proportional to the suspension voltage. Null bias error is reduced when the instrument is in orbit by reducing the suspension force. For despun orbit data, accelerations due to bias must be separated from those due to drag for accurate density computation. In the elliptical orbit phase of the AE missions, bias values have been deduced from the sensor output obtained at altitudes where aerodynamic drag is negligible. Bias measurements obtained from all three satellites are summarized. A bias temperature coefficient is also calculated. Results in this report show that orbital values differ from a simple extrapolation of the ground calibration data. This difference must be known to obtain accurate density data above about 200 km. The orbital bias results are applied to improve the accuracy of despun orbit measurements made during both the elliptical and circular orbit phases of the AE mission. Methods of extending bias determination to circular orbit data are discussed. (Author)

Orbital Bias Determination for Accelerometers on Atmospheric Explorer Satellites

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Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (113 download)

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Book Synopsis Orbital Bias Determination for Accelerometers on Atmospheric Explorer Satellites by : Frank A. Marcos

Download or read book Orbital Bias Determination for Accelerometers on Atmospheric Explorer Satellites written by Frank A. Marcos and published by . This book was released on 1977 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive amount of neutral density data has been obtained from the highly successful accelerometer experiments on the Atmosphere Explorer -C, -D, and -E satellites. The accelerometer is electrostatically suspended and force rebalanced. Ground calibration requires sufficient suspension force to operate in the earth's 1g field. An important characteristic of the instrument is its null bias which is proportional to the suspension voltage. Null bias error is reduced when the instrument is in orbit by reducing the suspension force. For despun orbit data, accelerations due to bias must be separated from those due to drag for accurate density computation. In the elliptical orbit phase of the AE missions, bias values have been deduced from the sensor output obtained at altitudes where aerodynamic drag is negligible. Bias measurements obtained from all three satellites are summarized. A bias temperature coefficient is also calculated. Results in this report show that orbital values differ from a simple extrapolation of the ground calibration data. This difference must be known to obtain accurate density data above about 200 km. The orbital bias results are applied to improve the accuracy of despun orbit measurements made during both the elliptical and circular orbit phases of the AE mission. Methods of extending bias determination to circular orbit data are discussed. (Author).

The Launch and On-Orbit Operations of Boeing's GPS Satellites

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Publisher :
ISBN 13 : 9781082302978
Total Pages : 480 pages
Book Rating : 4.3/5 (29 download)

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Book Synopsis The Launch and On-Orbit Operations of Boeing's GPS Satellites by : Len Losik Ph D

Download or read book The Launch and On-Orbit Operations of Boeing's GPS Satellites written by Len Losik Ph D and published by . This book was released on 2019-07-23 with total page 480 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Launch and On-Orbit Operations of Boeing's GPS Satellites documents the design of the Boeing GPS Block I satellites and the author's work as Boeing's GPS Space and Ground Segment Manager when he developed and used predictive algorithms to identify premature aging in normal appearing engineering measurement telemetry from electrical and electro-mechanical equipment on Boeing/U.S. Air Force GPS satellites winning Boeing $4.5B in future GPS satellite contracts that was contractually documented in GPS monthly and quarterly orbital test reports as CDRLs. The author includes the results of the use of PHM analysis on the NASA/Orbital/Berkeley Extreme Ultra-Violet Explorer Low earth orbiting space science satellite, a sister ship to the NASA/Lockheed Hubble Space Telescope. Now called prognostics and health management or PHM, predictive algorithms in PHM were developed by the author and used on the Boeing/U.S. Air Force's GPS Block I space-based navigation satellites to nullify the lack of GPS satellite telemetry from each of the on-orbit GPS satellites. PHM was first used by the author in 1979 to predict on-board GPS satellite atomic frequency standard failures for replacement prior to system wide, multi-service testing on the initial GPS constellation of 12 Block I MEO satellites that were operating in a 12,000 mile altitude, inclined 63 degrees, in a circular Earth orbit for achieving the maximum navigation payload system performance that would justify funding the GPS program by the Department of Defense over two existing fully funded U.S. Navy satellite-based navigation systems. The 12 Boeing Block 1 GPS satellite constellation was used to win program funding by the author from the Department of Defense resulting in two follow-on contracts for a total of $4.5B for 28 additional Block II GPS satellites and 12 Block IIA and 12 Block IIF satellites with improvements over the Block I satellites based on the results from the author's routine prognostic analysis he completed to keep GPS satellite equipment and navigation payload performance and reliability as high as possible. With the Air Force's GPS program funded by the Department of Defense in 1981, the two existing, Navy satellite-based navigation and timing programs called TIMATION and TRANSIT were retired and the ownership of the Air Force's GPS program was turned over to the U.S. government for funding and operations after GPS was provided for public use for free by President Ronald Reagan in 1986 following the intentional shoot down of a commercial Korean airlines passenger jet over the Soviet Union by a Soviet Union fighter pilot. an Addendum has been added to illustrate the author's use of Fourier analysis to create virtual telemetry behavior for GPS satellite subsystem equipment telemetry that was not available due to the restrictions placed on each Boeing GPS satellite telemetry availability by senior Air Force officers at AFSMC (SAMSO) in Los Angeles CA. and Lockheed Missiles and Space Company management and AFSCF contracted satellite operations personnel in Sunnyvale CA., who wanted the GPS test and evaluation program to fail.

The Observatory

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ISBN 13 :
Total Pages : 892 pages
Book Rating : 4.:/5 (35 download)

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Book Synopsis The Observatory by :

Download or read book The Observatory written by and published by . This book was released on 2003 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A review of astronomy" (varies).

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1018 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1978 with total page 1018 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Travaux

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ISBN 13 :
Total Pages : 524 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Travaux by : International Association of Geodesy

Download or read book Travaux written by International Association of Geodesy and published by . This book was released on 1995 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Physics Briefs

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ISBN 13 :
Total Pages : 710 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Physics Briefs by :

Download or read book Physics Briefs written by and published by . This book was released on 1992 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Satellite Orbits

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Publisher : Springer Science & Business Media
ISBN 13 : 3642583512
Total Pages : 378 pages
Book Rating : 4.6/5 (425 download)

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Book Synopsis Satellite Orbits by : Oliver Montenbruck

Download or read book Satellite Orbits written by Oliver Montenbruck and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 378 pages. Available in PDF, EPUB and Kindle. Book excerpt: This modern presentation guides readers through the theory and practice of satellite orbit prediction and determination. Starting from the basic principles of orbital mechanics, it covers elaborate force models as well as precise methods of satellite tracking. The accompanying CD-ROM includes source code in C++ and relevant data files for applications. The result is a powerful and unique spaceflight dynamics library, which allows users to easily create software extensions. An extensive collection of frequently updated Internet resources is provided through WWW hyperlinks.

Radiometric Tracking Techniques for Deep-Space Navigation

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Publisher : John Wiley & Sons
ISBN 13 : 0471726168
Total Pages : 99 pages
Book Rating : 4.4/5 (717 download)

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Book Synopsis Radiometric Tracking Techniques for Deep-Space Navigation by : Catherine L. Thornton

Download or read book Radiometric Tracking Techniques for Deep-Space Navigation written by Catherine L. Thornton and published by John Wiley & Sons. This book was released on 2005-03-04 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: Radiometric Tracking Techniques for Deep-Space Navigation focuses on a broad array of technologies and concepts developed over the last four decades to support radio navigation on interplanetary spacecraft. In addition to an overview of Earth-based radio navigation techniques, the book includes a simplified conceptual presentation of each radiometric measurement type, its information content, and the expected measeurement accuracy. The methods described for both aquiring and calibrating radiometric measurements also provide a robust system to support guidance and navigation for future robotic space exploration.

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 934 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 934 pages. Available in PDF, EPUB and Kindle. Book excerpt:

GEOPHYSICS AND GEOCHEMISTRY – Volume III

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Publisher : EOLSS Publications
ISBN 13 : 1848262477
Total Pages : 454 pages
Book Rating : 4.8/5 (482 download)

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Book Synopsis GEOPHYSICS AND GEOCHEMISTRY – Volume III by : Jan Lastovicka

Download or read book GEOPHYSICS AND GEOCHEMISTRY – Volume III written by Jan Lastovicka and published by EOLSS Publications. This book was released on 2009-11-28 with total page 454 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geophysics and Geochemistry is a component of Encyclopedia of Earth and Atmospheric Sciences in the global Encyclopedia of Life Support Systems (EOLSS), which is an integrated compendium of twenty one Encyclopedias. Geophysics and Geochemistry are two closely intertwined and collaborating branches of Earth’s sciences. The content of the Theme on Geophysics and Geochemistry is organized with state-of-the-art presentations covering eight main topics: Foundations of Geophysics and Geochemistry; Geophysical Systems; Seismology and Volcanology; Geomagnetism and Geoelectricity; Aeronomy and Magnetosphere; Gravimetry; Geochemistry and Cosmochemistry; Planetology – Comparative Planetology of Earth-like Planets and Astrobiology which are then expanded into multiple subtopics, each as a chapter. These three volumes are aimed at the following a wide spectrum of audiences from the merely curious to those seeking in-depth knowledge: University and College students Educators, Professional practitioners, Research personnel and Policy analysts, managers, and decision makers and NGOs.