Astronomy and Astrophysics – Astronomy
Scientific paper
Aug 1984
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984adans..54..543a&link_type=abstract
IN: Astrodynamics 1983; Proceedings of the Conference, Lake Placid, NY, August 22-25, 1983. Part 1 (A84-30526 13-13). San Diego,
Astronomy and Astrophysics
Astronomy
Computer Programs, Ephemerides, Global Positioning System, Microcomputers, Orbit Calculation, Satellite Orbits, Interpolation, Orbit Perturbation, Orbital Elements, Orbital Mechanics, Polynomials, Radiation Effects
Scientific paper
In connection with MITES data reduction operations, the ephemerides for Global Positioning System (GPS) satellites are required. MITES is a system of miniature radio interferometer terminals for the measurement of baseline vectors on the ground by means of interferometric observations of GPS satellites. MITES employs the LSI-11 microprocessor with 64 KB of memory for the involved numerical operations, and it is, therefore, necessary to have for the calculation of the satellite ephemerides a model which will run on this microcomputer. The present investigation is concerned with the solution of this problem. Attention is given to a general description of the considered model, the partial derivatives, and the adaptation of a semianalytical orbit model, used on a larger computer, for the LSI-11 by means of an overlay structure.
Abbot Richard I.
Cefola P.
Tse S. F.
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