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Friday, May 15, 2020 | History

3 edition of Analytical derivation and verification of zero-gyro control for the IUE satellite found in the catalog.

Analytical derivation and verification of zero-gyro control for the IUE satellite

Tiffany Bowles

Analytical derivation and verification of zero-gyro control for the IUE satellite

by Tiffany Bowles

  • 128 Want to read
  • 9 Currently reading

Published by National Aeronautics and Space Administration, Goddard Space Flight Center in Greenbelt, MD .
Written in English

    Subjects:
  • IUE (Artificial satellite),
  • Artificial satellites -- Attitude,
  • Artificial satellites -- Attitude control systems

  • Edition Notes

    StatementTiffany Bowles and John Croft.
    SeriesNASA technical memorandum -- 100748.
    ContributionsCroft, John., Goddard Space Flight Center.
    The Physical Object
    Pagination1 v. (various pagings) :
    ID Numbers
    Open LibraryOL17630313M
    OCLC/WorldCa55129616


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Analytical derivation and verification of zero-gyro control for the IUE satellite by Tiffany Bowles Download PDF EPUB FB2

Analytical Derivation and Verification of Zero-Gyro Control for the IUE Satellite PREFACE The International Ultraviolet Explorer (IUE) satellite was launched Janu into a geosynchronous orbit over South America. From its stationary position, the telescope maintains continuous communication with the control centers at.

Get this from a library. Analytical derivation and verification of zero-gyro control for the IUE satellite. [Tiffany Bowles; John Croft; Goddard Space Flight Center.].

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Published: () Conceptual design of a synchronous Mars telecommunications satellite Published: (). Satellite communications payload and system by: Braun, T. M., Published: () Analytical derivation and verification of zero-gyro control for the IUE satellite by: Bowles, Tiffany.

The Small Scientific Satellite (S 3 or Explorer) was one of the first satellites of this decade. Launched on Novemits mission was to study the earth’s magnetosphere (see Fig. 10). It was a small, spin-stabilized satellite, with a launch mass of approximately 52 kg, and was placed in a highly elliptical orbit of km x 18, km at ° inclination.

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Zero-gyro control of the International Ultraviolet Explorer. NASA Technical Reports Server (NTRS) O'Donnell, James R., Jr.; Hoffman, Henry C. The IUE was built for an anticipated lifespan of three years with a goal of five. Long-term in vivo left ventricular assist device study for days with Gyro PI pump.

PubMed. Ohtsuka, G; Nakata, K; Yoshikawa, M; Takano, T; Glueck, J; Sankai, Y.