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

EECFI.AemMetadata Class Reference

Class for reading AEM files. More...

List of all members.

Public Member Functions

 AemMetadata ()
 Constructor.

Public Attributes

String comment
 Comments (metadata section).
String objectName
 The name of the object for which the ephemeris is provided.
String objectId
 Object identifier of the object for which the ephemeris is provided.
String centerName
 Origin of reference frame, which may be a natural solar system body (planets, asteroids, comets, and natural satellites), including any planet barycenter or the solar system barycenter, or another spacecraft (in this case the value for CENTER_NAME is subject to the same rules as for OBJECT_NAME).
String refFrameA
 Name of the reference frame for the origin/destiny of the atttitude transformation.
String refFrameB
 Name of the other reference frame for the origin/destiny of the atttitude transformation.
String attitudeDir
 Transformation direction A2B or B2A.
String timeSystem
 Time system used for metadata, ephemeris data, and covariance data.
String startTime
 Start of TOTAL time span covered by attitude data immediately following this metadata block.
String useableStartTime
 Optional start and end of USEABLE time span covered by attitude data immediately following this metadata block.
String useableStopTime
 Optional start and end of USEABLE time span covered by attitude data immediately following this metadata block.
String stopTime
 End of TOTAL time span covered by attitude data immediately following this metadata block.
String attitudeType
 Attitude data type: QUATERIONS, EULER_ANGLES.
String quaternionType
 Quaterion type.
String eulerRotSeq
 Euler rotation sequence.
String interpolation
 This keyword may be used to specify the recommended interpolation method for attitude data in the immediately following set of attitude lines.
String interpolationDegree
 Recommended interpolation degree for attitude data in the immediately following set of attitude lines.

Detailed Description

Class for reading AEM files.


Constructor & Destructor Documentation

EECFI.AemMetadata.AemMetadata (  ) 

Constructor.


Member Data Documentation

Transformation direction A2B or B2A.

Attitude data type: QUATERIONS, EULER_ANGLES.

Origin of reference frame, which may be a natural solar system body (planets, asteroids, comets, and natural satellites), including any planet barycenter or the solar system barycenter, or another spacecraft (in this case the value for CENTER_NAME is subject to the same rules as for OBJECT_NAME).

Comments (metadata section).

Euler rotation sequence.

This keyword may be used to specify the recommended interpolation method for attitude data in the immediately following set of attitude lines.

Recommended interpolation degree for attitude data in the immediately following set of attitude lines.

Object identifier of the object for which the ephemeris is provided.

The name of the object for which the ephemeris is provided.

Quaterion type.

Inidicates if the real part is the FIRST of the LAST element in the following data

Name of the reference frame for the origin/destiny of the atttitude transformation.

Name of the other reference frame for the origin/destiny of the atttitude transformation.

Start of TOTAL time span covered by attitude data immediately following this metadata block.

End of TOTAL time span covered by attitude data immediately following this metadata block.

Time system used for metadata, ephemeris data, and covariance data.

Optional start and end of USEABLE time span covered by attitude data immediately following this metadata block.

Optional start and end of USEABLE time span covered by attitude data immediately following this metadata block.


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