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
Published
1989
by National Aeronautics and Space Administration, Goddard Space Flight Center in Greenbelt, MD
.
Written in English
Edition Notes
Statement | Tiffany Bowles and John Croft. |
Series | NASA technical memorandum -- 100748. |
Contributions | Croft, John., Goddard Space Flight Center. |
The Physical Object | |
---|---|
Pagination | 1 v. (various pagings) : |
ID Numbers | |
Open Library | OL17630313M |
OCLC/WorldCa | 55129616 |
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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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Analytical derivation and verification of zero-gyro control for the IUE satellite eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA. Analytical derivation and verification of zero-gyro control for the IUE satellite by: Bowles, Tiffany.
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.