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Cross Pattern Fine Peaking Width
4
Float
0.0 - 60.0
Width in degrees to scan during a fine cross
pattern peaking function.
Cross Pattern Fine Peaking Height
4
Float
0.0 - 60.0
Height in degrees to scan during a fine cross
pattern peaking function.
Cross Pattern Fine Signal Tolerance
1
Float
0.0 to 1000.0
Signal degradation amount before a scan stops.
“Fine Cross Peaking” is an alternate method used by the AAQ for Fine Peaking on the received
satellite signal. As currently designed, this option must be requested by the customer before the
antenna leaves AvL.
The
Cross Pattern Fine Velocity
parameters specify the speed that the antenna will move in each
direction during the signal level measurement scans. As was true for the Scan Velocity parameters,
the possibly sluggish response time of the Signal Source and the desire for short Acquisition times
must be considered.
The
Cross Pattern Fine Peaking
parameters set the total AZ width and EL height of the “cross” that
will be scanned. These parameters should be set sufficiently large enough to insure that the peak of
the antenna’s Main Beam is included in the scan. However, making them overly large will add time
to the overall Acquisition process.
Cross Pattern Fine Signal Tolerance
sets a tolerance on acceptable signal drop between peaking
cycles. If this parameter value is exceeded, then the AAQ assumes that the satellite signal is
experiencing a Rain Fade and the peaking process is suspended.
6.5.6 Step Pattern Mode
Long name
Level
Type
Value Range
Documentation
Peaking Azimuth Travel
Limit
4
Float
0.1 - 100.0 (deg)
The maximum amount of degrees that the azimuth
axis can be moved during a single peaking cycle.
Peak Dwell Iterations
4
Unsigned
1 - 100
Number of peaking iterations to look for signal
changes.
Peaking Elevation Travel
Limit
4
Float
0.1 - 100.0 (deg)
The maximum amount of degrees that the elevation
axis can be moved during a single peaking cycle.
Peaking Travel Limit
parameters set a maximum limit on AZ and EL travel during the Step Peaking
process. This way a reasonable search area can be defined that prevents the system from peaking
on noise for an extended period of time should a weak satellite signal be lost during the Step
Peaking process. When one of these limits is exceeded, Step Peaking is terminated and a message is
displayed in the GUI.
Peak Dwell Iterations
defines the number of signal measurements that will be averaged to
determine the pointing metric for that particular step and hence the dwell time at the end of each