TECHNICAL DESCRIPTION INTRAC-305
Page 58 INTRAC-305 MANUAL - Issue 3.2 © 2011 Advantech Wireless
within the soft limits?). If they are invalid the INTRAC sets the
maximum possible angle(s) in the required direction and
prompts the operator for action. If the co-ordinates are valid
the INTRAC drives the antenna to those co-ordinates and
enters Standby. The antenna can then be peaked using
manual mode or search mode (see below) before selecting
Auto New Model.
Note If Auto Continue is selected at the end of Goto and there is a
model in existence the INTRAC will continue to track using that
model. To commence learning a new orbit either Auto New
Model should be selected or any existing model cleared before
selecting Auto Continue.
Goto Satellite This mode allows one of the previously programmed satellites
(up to 40 can be programmed) to be selected by number and
its position driven to. Using the “Edit Satellite” sub menu of the
Goto Satellite menu a new satellite can be added or an existing
one edited. Having selected the required satellite pressing the
enter key causes the antenna to be driven to that satellite. The
INTRAC enters Standby when the antenna is at the satellite’s
position. Antenna position peaking can then be carried out
manually or in search mode (see below). To commence
tracking this new satellite select Auto New Model or if there is
no existing model Auto Continue may be selected. (see Note
above)
Search Search Mode conducts a search of the sky based on
parameters entered in this menu. When the menu is entered
the displayed parameters are those of the current antenna
pointing. e.g. the parameters from a Goto move. If these
parameters are not those required they may be edited in this
menu. (see page 21)
The search box size angles are plus and minus on the nominal
angle. Thus entering 2 by 2 would cause a search box of 4
square.
The search begins in the nearest corner of the defined box to
the antenna’s current pointing. The search pattern is a “toast
rack” or “serpent shape. The scanning comprises full scans in
elevation for each move in azimuth. The azimuth move is
equal to the 3dB beamwidth of the antenna commencing 1/2 of
the 3dB beamwidth in from the edge of the box.
The position of the highest beacon signal strength during these
scans is recorded. At the end of the “serpentine” search the
antenna is driven to the point of highest signal strength found
during those scans and phase two of the search is
commenced.
This is the peaking phase and causes the antenna to search a
smaller area of sky around the point of highest signal strength
for the peak level. Again the position of the highest signal