Eg.
- Code: Select all
<vacuum>
<name>vacuum</name>
<number>0</number>
<rpm>systems/electrical/outputs/ac-main-voltage</rpm>
<scale>25.0</scale>
</vacuum>
But it seem that its hard to get the AI to work above approx 12 000 m regardless of the scale factor used to drive it due to the low air pressure.
The advantage of using the standard AI is that it comes as a package with properties, calculations and instrument errors.
How to best solve this/or replace for an aircraft with a high ceiling (20 000 m)?