ORBIT DETERMINATION MODELING ANALYSIS BY GPS INCLUDING PERTURBATIONS DUE TO GEOPOTENTIAL COEFFICIENTS OF HIGH DEGREE AND ORDER, SOLAR RADIATION PRESSURE AND LUNI-SOLAR ATTRACTION. doi: 10.5028/jatm.2011.03010611

ORBIT DETERMINATION MODELING ANALYSIS BY GPS INCLUDING PERTURBATIONS DUE TO GEOPOTENTIAL COEFFICIENTS OF HIGH DEGREE AND ORDER, SOLAR RADIATION PRESSURE AND LUNI-SOLAR ATTRACTION. doi: 10.5028/jatm.2011.03010611

The purpose of this paper was to analyze the modeling of an artificial satellite orbit, using signals of the GPS constellation and least squares algorithms as the method of estimation, with the aim of analyzing the performance of the orbit estimation process. One pursues to verify how difference...

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Bibliographic Details
Main Authors: Paula C. P. M. Pardal, Rodolpho Vilhena de Moraes, Helio K. Kuga
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2011-08-01
Series:Journal of Aerospace Technology and Management
Subjects:
Orbit determination
GPS
Orbit perturbations
Geopotential
Solar radiation pressure
Luni-solar gravitational attraction
Online Access:https://www.jatm.com.br/jatm/article/view/84

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