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...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Instituto de Aeronáutica e Espaço (IAE)
2011-08-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | https://www.jatm.com.br/jatm/article/view/84 |