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aircraft:tmd:turbo_engines [2021/02/12 13:14] – [Step 6 - Engine control (FADEC)] jhaircraft:tmd:turbo_engines [2022/08/02 10:00] (current) – jh
Line 27: Line 27:
  
 <code>            <[input_lever][Throttle1Input][] <code>            <[input_lever][Throttle1Input][]
-                <[string8][Input][Controls.Throttle1]>+                <[string8][Message][Controls.Throttle1]>
             >             >
             <[turbofan][Engine1][]             <[turbofan][Engine1][]
Line 73: Line 73:
 <code>            // engine controls <code>            // engine controls
             <[input_lever][Throttle1Input][]             <[input_lever][Throttle1Input][]
-                <[string8][Input][Controls.Throttle1]>+                <[string8][Message][Controls.Throttle1]>
             >             >
             <[constant][Reverser1Flaps][]             <[constant][Reverser1Flaps][]
Line 457: Line 457:
 Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ). Enrichment = Engine1Station3.OutputTotalPressure / ( PitotTube.StaticPressure * DesignCompressionRatio ).
  
-FuelFlowRaw = C_FF * ( Governor + Enrichment )+Gain = PitotTube.StaticPressure / 101325.0 
 + 
 +FuelFlowRaw = Gain * C_FF * ( Governor + Enrichment )
  
 FuelFlow = clamp( FuelFlowRaw, MinFuelFlow, MaxFuelFlow )</code> FuelFlow = clamp( FuelFlowRaw, MinFuelFlow, MaxFuelFlow )</code>
aircraft/tmd/turbo_engines.1613132074.txt.gz · Last modified: 2021/02/12 13:14 by jh