January 26, 2009:
Data prepared for the September 26, 2008 flight test.
File name: 20080926_lvrsol_13500s.
Duration: 13500 seconds.
Description:
Contains the time history of the ECEF position of the upper and lower reflectors 
on the Cesna aircraft.  Position is derived by using the precise, kinematic 
DGPS solution and adding to it the lever arm between the GPS antenna and the 
reflector rotated using either the C-Migits IMU or the Novatel Spann IMU.

Format: 
GPS_J2000: GPS seconds since J2000
CmigLowRefX: X Position in ECEF in km of the lower reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
CmigLowRefY: Y Position in ECEF in km of the lower reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
CmigLowRefZ: Z Position in ECEF in km of the lower reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
CmigUpRefX:  X Position in ECEF in km of the upper reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
CmigUpRefY:  Y Position in ECEF in km of the upper reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
CmigUpRefZ:  Z Position in ECEF in km of the upper reflector using the 
	     C-Migits IMU to perform the lever arm transformation. 
NovLowRefX:  X Position in ECEF in km of the lower reflector using the 
	     Novatel Span IMU to perform the lever arm transformation. 
NovLowRefY:  Y Position in ECEF in km of the lower reflector using the 
	     Novatel Span IMU to perform the lever arm transformation. 
NovLowRefZ:  Z Position in ECEF in km of the lower reflector using the 
	     Novatel Span IMU to perform the lever arm transformation. 
NovUpRefX:   X Position in ECEF in km of the upper reflector using the 
	     Novatel Span IMU to perform the lever arm transformation. 
NovUpRefY:   Y Position in ECEF in km of the upper reflector using the 
	     Novatel Span IMU to perform the lever arm transformation. 
NovUpRefZ:   Z Position in ECEF in km of the upper reflector using the 
	     Novatel Span IMU to perform the lever arm transformation.