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T0: 12\13\2015 7:34:0.07 GMT

Launcher Settings:
==================

Launcher: ASC Athena
Latitude: 69.2942 Degrees
Longitude: 16.0193 Degrees
Altitude: 171.3 Feet
Elevation: 80.28 Degrees
Azimuth: 12.08 Degrees
Bank: 0 Degrees

Attitude Output:
==================

time: Seconds from T0, reference above
roll: Euler rotation angle* (degrees) about the longitudinal geometric axis, X, through the nose (FWD)
yaw: Euler rotation angle* (degrees) about lateral axis, Z, at 180 degrees from the rail
pitch: Euler rotation angle* (degrees) about the lateral axis, Y, at 90 degrees from the rail
roll_rate: Roll rate (about the spin axis, X) in cycles/second (Hz)
a11: Element 1 (row 1, column 1) of 'ENU'**
a12: Element 2 (row 1, column 2) of 'ENU'**
a13: Element 3 (row 1, column 3) of 'ENU'**
a21: Element 4 (row 2, column 1) of 'ENU'**
a22: Element 5 (row 2, column 2) of 'ENU'**
a23: Element 6 (row 2, column 3) of 'ENU'**
a31: Element 7 (row 3, column 1) of 'ENU'**
a32: Element 8 (row 3, column 2) of 'ENU'**
a33: Element 9 (row 3, column 3) of 'ENU'**
X_Az: Azimuth of spin axis (degrees), X, from the fixed, local geodetic, East, North, Up (ENU) reference frame
X_El: Elevation of spin axis (degrees), X, from the fixed, local geodetic, East, North, Up (ENU) reference frame
Y_Az: Azimuth of lateral axis (degrees), Y, from the fixed, local geodetic, East, North, Up (ENU) reference frame
Y_El: Elevation of lateral axis (degrees), Y, from the fixed, local geodetic, East, North, Up (ENU) reference frame
Z_Az: Azimuth of lateral axis (degrees), Z, from the fixed, local geodetic, East, North, Up (ENU) reference frame
Z_El: Elevation of lateral axis (degrees), Z, from the fixed, local geodetic, East, North, Up (ENU) reference frame
F_az: Azimuth of payload velocity vector (degrees), from the fixed, local geodetic, East, North, Up (ENU) reference frame
F_el: Elevation payload velocity vector (degrees), from the fixed, local geodetic, East, North, Up (ENU) reference frame
latg: Geodetic latitude of the payload, in degrees
long: Geodetic longitude of the payload, in degrees
alt:  Altitude, in meters

Position Source: GPS
================

Attitude Source: GLNMAC
================

* Euler angles are body to reference (defined above) in a 3-2-1 sequence 

** 'ENU' is a 3x3xn direction cosine matrix representing rotation from the payload frame 
to the 'ENU' reference frame, where the payload frame is defined by X (column 1) pointing FWD 
through the payload spin axis, Y (column 2) through payload 90 degrees, and Z (column 3) through payload
180 degrees, where payload 0 degrees points towards the rail and increases in a clockwise
direction looking forward (through the nose).  The 'ENU' reference is the local geodetic 
East, North, Up, coordinate frame.