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SPACE TRACK. SPACE VEHICLE EPHEMERIS AND DIFFERENTIAL CORRECTION PROGRAM UNIFIED THEORY

PHILCO NEWPORT BEACH CA AERONUTRONIC DIV

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Título:
SPACE TRACK. SPACE VEHICLE EPHEMERIS AND DIFFERENTIAL CORRECTION PROGRAM UNIFIED THEORY
Autor: PHILCO NEWPORT BEACH CA AERONUTRONIC DIV
Assuntos: ARTIFICIAL SATELLITES ; Celestial Mechanics ; MATHEMATICAL ANALYSIS ; ORBITS ; SPACE PROBES ; SPACECRAFT ; Unmanned Spacecraft
Notas: DTIC AND NTIS
Descrição: An outline is given on the development of a differential correction theory for lunar and space probes. To overcome the singularities inherent in differential processes with conventional two-body descriptions of the path, as the eccentricity passes through unity in either the parabolic or rectilinear sense, a unified formulation of the two-body equations was developed. The differential correction procedure (over) is based upon an ephemeris, integrated in Encke form by special perturbations, and upon differential expressions derived from the unified two-body equations. The report includes experimentation with simulated range, range-rate, azimuth, altitude, right ascension and/or declination data to evaluate the performance of the resulting IBM 709 program. AFCCDD-TN-60-34 (Air Force Command and Control Development Division)
Data de criação/publicação: 1960
Idioma: Inglês

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