Ground proximity warning system: Difference between revisions

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Mode 6 (bank angle and altitude above field callouts) depends on a serviceable attitude reference, and ideally a valid decision height. <tt>/instrumentation/attitude-indicator/indicated-roll-deg</tt> is the key attitude property, which comes from either the attitude indicator (which is vacuum powered) or the master reference gyro (which is electrically powered).  
Mode 6 (bank angle and altitude above field callouts) depends on a serviceable attitude reference, and ideally a valid decision height. <tt>/instrumentation/attitude-indicator/indicated-roll-deg</tt> is the key attitude property, which comes from either the attitude indicator (which is vacuum powered) or the master reference gyro (which is electrically powered).  


==External links==
* Docs by original developer [http://www.mail-archive.com/flightgear-devel@lists.sourceforge.net/msg01902.html 1] [http://www.mail-archive.com/flightgear-devel@lists.sourceforge.net/msg01902/mk-viii-manual.tgz 2]


[[Category:Aircraft enhancement]]
[[Category:Aircraft enhancement]]

Revision as of 15:10, 17 September 2009

This article is a stub. You can help the wiki by expanding it.

Ground proximity warning system (GPWS) is a system designed to alert pilots if their aircraft is in immediate danger of flying into the ground or an obstacle. Another common name for such a system is ground-collision warning system (GCWS).

Add to an aircraft

Add this code to your -set.xml file (above the </sim> tag), to make the GPWS operatable, set instrumentation/mk-viii/servicable to true.

<instrumentation>
 <mk-viii>
  <name>mk-viii</name>
  <number>0</number>
 </mk-viii>
</instrumentation>

The MkVIII depends on many other systems, which must also be configured correctly, or it will behave unexpectedly.

Mode 6 (bank angle and altitude above field callouts) depends on a serviceable attitude reference, and ideally a valid decision height. /instrumentation/attitude-indicator/indicated-roll-deg is the key attitude property, which comes from either the attitude indicator (which is vacuum powered) or the master reference gyro (which is electrically powered).

External links

  • Docs by original developer 1 2