DEIMOS
Earth Observation Mission CFI Software
Orbit Software User Manual
for JAVA
ESA

Class List

Here are the classes, structs, unions and interfaces with brief descriptions:
EECFI.ANXExtraANX extra information
EECFI.AnxInfoAscending node information
EECFI.ANXTimeThis class contains a time instant given as an absolute orbit number plus the time elapsed since the ANX
EECFI.CheckOefOEF file check result
EECFI.EnumOrbitEnumerations for Orbit library
EECFI.GeoGeodCoordGeostationary orbit information
EECFI.GeoOrbitInfoGeostationary orbit information
EECFI.GeoOrbitInitDataGeostationary orbit init information
EECFI.OrbitalInfoOrbital information
EECFI.OrbitChangeDataChange orbit number in orbit id
EECFI.OrbitChangeFileChange orbit number in orbit id
EECFI.OrbitDataFilterConfigurationGeneral Data Filter Configuration
EECFI.OrbitDataFilterOutliersConfigurationOutliers Data Filter Outliers Configuration
EECFI.OrbitDataFilterOutliersReportOutliers Data Filter Outliers Report
EECFI.OrbitDataFilterOutputGeneral Data Filter Output
EECFI.OrbitDataFilterReportGeneral Data Filter Report
EECFI.OrbitFuncClass grouping several static functions
EECFI.OrbitIdClass that stores the orbit data
EECFI.OrbitIdCheckReportClass that stores orbit diagnostic data
EECFI.OrbitInfoInformation of orbits
EECFI.OrbTimeTime container
EECFI.OrbTimeIntervalVisibility time interval
EECFI.OsfRecordsOrbital changes records
EECFI.RefOrbitInfoReference orbit information
EECFI.RelANXTimeThis class contains a time instant given as a relative orbit number plus the time elapsed since the ANX
EECFI.RelTimeSegmentThis class contains a time interval given by a start RelANXTime and a stop RelANXTime
EECFI.SecMicrosecClass to transform an input double value in seconds to seconds and microseconds in long format
EECFI.StateVectorExtraInfoExtra information of state vector
EECFI.StateVectorInfoInformation of state vector
EECFI.TimeSegmentThis class contains a time interval given by a start ANXTime and a stop ANXTime
EECFI.ValidityTimeValidity time

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