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Piper PA34-200T Seneca II: Difference between revisions
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→Full functional 3d cockpit
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=== Full functional 3d cockpit === | === Full functional 3d cockpit === | ||
[[Image:SenecaII_cockpit.jpg|thumb|left|The 3d cockpit]] | [[Image:SenecaII_cockpit.jpg|thumb|left|The 3d cockpit]] | ||
Allmost all controls, switches, gauges and indicators are implemented and functional in the cockpit. | Allmost all controls, switches, gauges and indicators are implemented and functional in the cockpit. For description of the panel have a look at the [[Seneca II Panel Reference]]. | ||
<br clear="all" /> | <br clear="all" /> | ||
=== Structural Icing === | === Structural Icing === | ||
Since the Seneca provides anti- and deice equipment, I tried to model structural icing into flightgear. A little nasal script does most of the work: First it reads the property nodes under /sim/model/icing where any number of iceable elements configure the ice sensitive elements of the aircraft. Each element have a name, a sensitivity to icing, may have a salvage control and the name of a output property where the collected amount of ice is written to. After the initial configuration, a timed loop is executed every 2 seconds. It | Since the Seneca provides anti- and deice equipment, I tried to model structural icing into flightgear. A little nasal script does most of the work: First it reads the property nodes under /sim/model/icing where any number of iceable elements configure the ice sensitive elements of the aircraft. Each element have a name, a sensitivity to icing, may have a salvage control and the name of a output property where the collected amount of ice is written to. After the initial configuration, a timed loop is executed every 2 seconds. It | ||