Orbit determination of highly elliptical Earth orbiters using improved Doppler data-processing modes

A navigation error covariance analysis of four highly elliptical Earth orbits is described, with apogee heights ranging from 20,000 to 76,800 km and perigee heights ranging from 1,000 to 5,000 km. This analysis differs from earlier studies in that improved navigation data-processing modes were used...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Estefan, J. A.
Format:	Report
Sprache:	eng
Schlagworte:	Astrodynamics
Online-Zugang:	Volltext bestellen
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