This paper presents the results obtained in the estimation of the state vector and in the parameter estimation of a linear model of the European satellite GEOS. The proposed method is the sequential decision technique based on a binary quantization procedure. This method is tested with simulated data as well as with in-flight data provided by telemetry.
Partitioning filter applications to European satellite GEOS
Trennfilteranwendungen fuer den Europaeischen Satelliten GEOS
1983
2 Seiten, 5 Quellen
Conference paper
English
RAUMFAHRTTECHNIK , SATELLITENUEBERTRAGUNG , SATELLITENBAHN , LAGEREGELUNG , GEOWISSENSCHAFT , FILTERTHEORIE , PARAMETERSCHAETZUNG , PARAMETERIDENTIFIKATION , MODELLUNTERSUCHUNG , TELEMETRIE , BINAERCODE , ANTENNENANLAGE , MATHEMATISCHES MODELL , NUMERISCHES VERFAHREN , DYNAMISCHES VERHALTEN , KALMAN-FILTER
GEOS-I Satellite Applications Briefing
NTRS | 1994
An apogee boost motor for the Geos European satellite
AIAA | 1975
|Multilaterating the GEOS-3 satellite
NTRS | 1977
|