5
Table 1-1.  SGA Performance Characteristics 
Parameter Characteristic 
Gimbal type  Elevation over azimuth, two axes of freedom 
Field of regard 
360 continuous in both axes 
Stabilization 
Three rate sensors, two axes, stabilization at 
Nadir 
Power consumption 
200 watts average @ 28 Volts, Direct 
Current (VDC), operating 
Weight 28.3 lbs. 
Size  9 inches diameter x 15.2 inches height 
Slew rates 
0 to 65 per second in both axes 
Position accuracy  3 arc minutes 
Kmax Acceleration 
60sec/sec both axes 
1.4.1.1 Gyro Stabilization 
Stabilization is an essential part of the SeaFLIR II Imaging System.  
Vibration and movement of the host platform can make viewing and 
tracking targets difficult and even impossible.  This is especially true 
when the system is in the narrow field of view.  The SeaFLIR II Imaging 
System uses three rate-sensitive fiber-optic-gyros (FOG) (2 azimuth and 
1 elevation) to compensate for vibration and motion of the host platform. 
All gyros provide analog outputs.  The amplitude of these outputs 
corresponds to any rate or motion imparted to the gyro(s).  Each gyro’s 
analog signal is conditioned in the SGA and sent to the CEU as an error 
signal.  The error signal is used by servo control circuitry to create a 
drive voltage for the respective torque motor.  The torque motors 
stabilize the SGA in two axes, azimuth and elevation.  The rate gyros 
used are fiber-optic-gyros with no spinning masses that are subject to life 
limitations.  The rate gyros do experience drift caused by electronic and 
thermal changes over time.  This appears as a command for the Gimbal 
to slew.  To reduce this effect, a gyro null circuit has been incorporated 
into the SeaFLIR II Imaging System.  The drift effect may be noticed 
during initial system start-up. When this occurs, the operator has the 
option to use either manual or activate an automatic null feature, to 
cancel out the gyro drift.  See paragraph 3.1.7 for the Gyro NULL 
function. 
Commercial in Confidence
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Retrieval Date:07-Dec-10
Requested by Bower,  Richard