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Nesis III User's Manual
combination allows optimal setting of power level. Gyroplanes and he-
licopters have rotors and in this case engine RPM is usually combined
with rotor RPM. See also section 3.11.4 on page 42.
○
The moving map provides basic navigation information. It is located
6
below the artificial horizon. The moving map can be configured to follow
aircraft true heading, tracking or magnetic heading. This map can be
also replaced with a direction indicator (see page 47). A touch on the
moving map window will switch to navigation screen.
○
The vertical speed indicator. The indicator can be combined with g-
7
meter (acceleration) located below the center.
○
The mini engine window organizes all most important engine parameters
8
into one simple colored bar based map. Each bar corresponds to one
parameter and the color of the bar to its current status. See also section
3.11.7 on page 45. Alternatively, an airplane designation can be shown
instead.
○
The fuel computer window provides the fuel and economy information.
9
Level of the fuel in tank, current and average fuel consumption, approx-
imate range and endurance. This monitor can be also replaced with
some other windows. See also section 3.11.8 on page 46.
3.7
Navigation Screen
The navigation screen is a large moving map combined with some additional
information. Large compass scale and vertical airspace situation are painted
over the map.
3.7.1
Main Elements of the Navigation Screen
Figure 6 illustrates an example and defines the main elements of the screen.
○
Status bar. This bar is shown on the top of most screens. Please refer
1
to section 3.4 on page 21 for more details.
○
Wind indication. This indication is available only when MAGU (elec-
2
tronic magnetic compass) is also present on the CAN bus.
3.7 Navigation Screen
27
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