PlatformCreate

Create a Platform file from scratch by defining attributes such as markerName, markerNumber, comment, approxPosition, equipment.

See also GnssAntex2AntennaDefinition and GnssStationLog2Platform.

Name	Type	Annotation
outputfilePlatform	filename
markerName	string
markerNumber	string
comment	string
approxPositionX	double	[m] in TRF
approxPositionY	double	[m] in TRF
approxPositionZ	double	[m] in TRF
equipment	choice
gnssAntenna	sequence
name	string
serial	string
radome	string
comment	string
timeStart	time
timeEnd	time
positionX	double	[m] ARP in north, east, up or vehicle system
positionY	double	[m] ARP in north, east, up or vehicle system
positionZ	double	[m] ARP in north, east, up or vehicle system
rotationX	angle	[degree] from local/vehicle to left-handed antenna system
rotationY	angle	[degree] from local/vehicle to left-handed antenna system
rotationZ	angle	[degree] from local/vehicle to left-handed antenna system
flipX	boolean	flip x-axis (after rotation)
flipY	boolean	flip y-axis (after rotation)
flipZ	boolean	flip z-axis (after rotation)
gnssReceiver	sequence
name	string
serial	string
version	string
comment	string
timeStart	time
timeEnd	time
laserRetroReflector	sequence
name	string	e.g. GFZ, ITE, IPIE
serial	string
comment	string
timeStart	time
timeEnd	time
positionX	double	[m] optial reference point RP in satellite system
positionY	double	[m] optial reference point RP in satellite system
positionZ	double	[m] optial reference point RP in satellite system
rotationX	angle	[degree] from local/vehicle to LRR system
rotationY	angle	[degree] from local/vehicle to LRR system
rotationZ	angle	[degree] from local/vehicle to LRR system
flipX	boolean	flip x-axis (after rotation)
flipY	boolean	flip y-axis (after rotation)
flipZ	boolean	flip z-axis (after rotation)
range	double	[m] range bias (only without range matrix)
inputfileRangeMatrix	filename	[m] (azimuth(0..360) x zenith(0..dZenit*rows)
dZenit	angle	[degree] increment of range matrix
geodeticSatellite	sequence	e.g. LAGEOS
name	string
serial	string
comment	string
timeStart	time
timeEnd	time
range	double	[m] standard center-of-mass correction
slrStation	sequence
name	string	CDP SOD 8-digit No.
serial	string	IERS DOMES
comment	string
timeStart	time
timeEnd	time
positionX	double	[m] eccentricity in north
positionY	double	[m] eccentricity in east
positionZ	double	[m] eccentricity in up
satelliteIdentifier	sequence
name	string
serial	string
cospar	string	Satellite COSPAR ID
norad	string	Satellite Catalog (NORAD) Number
sic	string	SIC Code
sp3	string	SP3
comment	string
timeStart	time
timeEnd	time
other	sequence
name	string
serial	string
comment	string
timeStart	time
timeEnd	time
positionX	double	[m] in north, east, up or vehicle system
positionY	double	[m] in north, east, up or vehicle system
positionZ	double	[m] in north, east, up or vehicle system
referencePoint	sequence	e.g. center of mass in satellite frame
comment	string
xStart	double	[m] in north, east, up or vehicle system
yStart	double	linear motion between start and end
zStart	double
xEnd	double	[m] in north, east, up or vehicle system
yEnd	double	linear motion between start and end
zEnd	double
timeStart	time
timeEnd	time