C.Plath NAVIGAT X MK 1 Mod. 10, Руководство оператора

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Page 4-03
NAVIGAT X MK 1 Mod. 10 / SR-180 MK 1 Mod. 10
056310
3-149 MK110ENG.P65
4.3 Installation of the Gyrosphere
Install the gyrosphere as described under 5.3.3.
Note: The gyrosphere may be installed by personnel of an authorized C. PLATH
service station only.
4.4 Basic System Configuration
When the ship's cables have been connected and the gyrosphere installed, the basic
system configuration is to be carried out by setting the configuration parameters to
the required values in the service setup 1 (see 4.6).
To configure the system:
1) Go to the service setup 1 menu.
2) Select the required system type and heading reference selection mode (see
4.6.5). In twin gyrocompass systems, assign a compass ID (see 4.6.9).
3) Select the required data formats for all devices connected to the data inputs
(see 4.6.2). Disable unused heading inputs (gyro and/or magnetic hdg. in-
puts in system types G, GM, or GG).
4) Select the required data output formats (see 4.6.2).
5) If required, set the parameters for the analogue rate of turn output and the
rudder angle feedback and ext. status inputs.
Note: Do not change the preset shaft correction angle in the service setup 1. The
alignment error correction may be set to an approximate value at this point.
The existing alignment error, however, must be exactly determined and cor-
rected as described in the following section.
To round off the configuration:
1) Select the required speed/latitude modes, north speed error correction, voy-
age data printer and rate of turn output settings in the manual settings menu.
2) Enter the current date and time in the user setup menu.
Note: In twin gyrocompass systems, the individual compasses must be configured
separately with identical parameters except for the compass ID.
After configuration, function-check the complete system with all connected equip-
ment in operation. Use the test mode in the service setup 1 to check the heading
output to serial and 6 step/° repeaters and the analogue rate of turn output.
In order to bring the gyrocompass system into a working state, the existing alignment
error must now be determined and corrected as described in the following section.
If required, correction values for the magnetic compass heading display may be de-
termined and entered into the system's calibration table as described under 4.5.