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June 29, 2017
2.1 ALIGN Calibration Procedure
1. Create a text files with commands that specify IMU orientation, IMU type, and lever arms
between the IMU centre of navigation and both antennas.
In the following example, the IMU is an LN200 setup in the default way (z-axis pointing upwards,
Y-axis pointing forward) with the lever arms measuring the distance separation between the IMU
centre of navigation and each antenna. Modify the values shown in red accordingly to match your
setup.
CONNECTIMU COM1 LN200
SETINSROTATION RBV 0 0 0
SETINSTRANSLATION ANT1 0.8 -0.30 1.45 0.05 0.05 0.05
SETNINSTRANSLATION ANT2 -0.8 -0.30 1.45 0.05 0.05 0.05
2. Once you have a clear view of the sky and the SPAN system is powered on, copy/paste each of the
commands from step 1 into the Console Window in NovAtel Connect. The INS should align within
a few seconds through the aided-transfer INS alignment method (i.e: dual GNSS antenna).
3. Apply motion in order to converge INS error estimates
Apply figure 8 motion until the INS solution status has changed from
INS_ALIGNMENT_COMPLETE to INS_SOLUTION_GOOD.
4. Send the following command: LOG INSCALSTATUS ONCHANGED
The command above will output the INSOFFSETS message which can be used to monitor the
status of the ALIGN (boresight) calibration.
5. Send the following command to start the ALIGN calibration:
INSCALIBRATE ALIGN NEW < StdDev>
Where < StdDev> represents the standard deviation (in degrees) at which the ALIGN calibration
can stop. Suggested value is 0.3 degrees. The smaller the standard deviation value, the longer the
calibration. Recall the boresight calibration computes the angle between the SPAN computation
frame and the dual antenna baseline.
6. You should now notice the INSCALSTATUS message is output indicating the start of the ALIGN
calibration. If the INS hasn’t been converged enough (i.e: more initial kinematics are required),