Owner`s manual

On maps with grid systems there might be a need for using the grid north lines as North
reference. Select GRID NORTH if required.
Read more about reference systems in section 9.
7.1-8 SHOW XTE (Cross Track Error)
XTE is the distance traveled off of the intended direction of travel
(Fig. 13). Press YES, in XTE setting, to view Cross Track Error, in
the GPS navigation function. XTE is useful for times when you want
to leave the original course and need to get back on course again.
7.1-9 DEGREES/MILS/GON
Default setting for the TrueMagnetic compass is 360 degrees.
Military forces, NATO and others use 6400 MILS. The Swedish army uses 6300 mils.
Select the graduation you wish to use, DEGREES (360), MILS 640 (6400), MILS 630
(6300), MILS 600 (6000) or 400 GON (400).
7.1-10 SOFTWARE VERSION
View the software version and the number of your Multi-Navigator.
7.1-11 DELETE ALL WPTS
This function deletes the ENTIRE waypoint memory, plus ALL stored routes! Do not
enter, unless you want to delete all stored waypoints!
7.1-12 LANGUAGE
To change the language used by the Multi-Navigator press SET, and the display shows
the current language. Scroll through the languages using the UP/DOWN button. Select
the language of choice by pressing SET. Exit the language setting by pressing ESC.
7.2 -- POSITION SIDE FUNCTIONS & SETTINGS
7.2-1 SIDE FUNCTIONS
There are 2 side functions related to the Position function. (Fig. 14)
These are reached while pressing LEFT or RIGHT while in the POSITION function.
GPS ELEV Side Function
This is the elevation calculated by the GPS receiver, normally accurate to within 15
meters (49 feet). The graphic indicator shows rate of ascent/descent (each segment
indicates a rate of 1 meter/second).
SATELLITE STATUS Side Function
ACQUIRE indicates unit is collecting satellite data, but has not yet determined a position.
3D NAV or 2D NAV indicates the GPS receiver has determined your position. If GPS OFF
is shown, the GPS receiver has been shut off.
7
Figure 13
START
WPT
X
TE
You
GPS ELEV
Side Function
SATELLITE STATUS
Side Function
POSITION
Main Function
Figure 14