#### piston engine electrical system #### #### Syd Adams #### var ammeter_ave = 0.0; var outPut = "systems/electrical/outputs/"; var BattVolts = props.globals.getNode("systems/electrical/batt-volts",1); var Volts = props.globals.getNode("/systems/electrical/volts",1); var Amps = props.globals.getNode("/systems/electrical/amps",1); var EXT = props.globals.getNode("/controls/electric/external-power",1); var switch_list=[]; var output_list=[]; var watt_list=[]; #var battery = Battery.new(switch-prop,volts,amps,amp_hours,charge_percent,charge_amps); Battery = { new : func(swtch,vlt,amp,hr,chp,cha){ m = { parents : [Battery] }; m.switch = props.globals.getNode(swtch,1); m.switch.setBoolValue(0); m.ideal_volts = vlt; m.ideal_amps = amp; m.amp_hours = hr; m.charge_percent = chp; m.charge_amps = cha; return m; }, apply_load : func(load,dt) { if(me.switch.getValue()) { var amphrs_used = load * dt / 3600.0; var percent_used = amphrs_used / me.amp_hours; me.charge_percent -= percent_used; if ( me.charge_percent < 0.0 ) { me.charge_percent = 0.0; } elsif ( me.charge_percent > 1.0 ) { me.charge_percent = 1.0; } var output =me.amp_hours * me.charge_percent; return output; } else { return 0; } }, get_output_volts : func { if ( me.switch.getValue() ) { var x = 1.0 - me.charge_percent; var tmp = -(3.0 * x - 1.0); var factor = (tmp*tmp*tmp*tmp*tmp + 32) / 32; var output =me.ideal_volts * factor; return output; } else { return 0; } }, get_output_amps : func { if (me.switch.getValue() ) { var x = 1.0 - me.charge_percent; var tmp = -(3.0 * x - 1.0); var factor = (tmp*tmp*tmp*tmp*tmp + 32) / 32; var output =me.ideal_amps * factor; return output; } else { return 0; } } }; # var alternator = Alternator.new(num,switch,rpm_source,rpm_threshold,volts,amps); Alternator = { new : func (num,switch,src,thr,vlt,amp){ m = { parents : [Alternator] }; m.switch = props.globals.getNode(switch,1); m.switch.setBoolValue(0); m.meter = props.globals.getNode("systems/electrical/gen-load["~num~"]",1); m.meter.setDoubleValue(0); m.gen_output = props.globals.getNode("engines/engine["~num~"]/amp-v",1); m.gen_output.setDoubleValue(0); m.meter.setDoubleValue(0); m.rpm_source = props.globals.getNode(src,1); m.rpm_threshold = thr; m.ideal_volts = vlt; m.ideal_amps = amp; return m; }, apply_load : func(load) { var cur_volt=me.gen_output.getValue(); var cur_amp=me.meter.getValue(); if ( cur_volt >1 ) { var factor=1/cur_volt; gout = (load * factor); if ( gout>1 ) { gout=1; } } else { gout=0; } if ( cur_amp > gout ) { me.meter.setValue(cur_amp - 0.01); } if ( cur_amp < gout ) { me.meter.setValue(cur_amp + 0.01); } }, get_output_volts : func { var out = 0; if ( me.switch.getBoolValue() ) { var factor = me.rpm_source.getValue() / me.rpm_threshold; if ( factor > 1.0 ) { factor = 1.0; } var out = (me.ideal_volts * factor); } me.gen_output.setValue(out); return out; }, get_output_amps : func { var ampout =0; if(me.switch.getBoolValue()){ var factor = me.rpm_source.getValue() / me.rpm_threshold; if ( factor > 1.0 ) { factor = 1.0; } ampout = me.ideal_amps * factor; } return ampout; } }; var battery = Battery.new("/controls/electric/battery-switch",24,30,34,1.0,7.0); var alternator1 = Alternator.new(0,"controls/electric/engine[0]/generator","/engines/engine[0]/rpm",100.0,28.0,60.0); alternator2 = Alternator.new(1,"controls/electric/engine[1]/generator","/engines/engine[1]/rpm",20.0,28.0,60.0); ##################################### setlistener("/sim/signals/fdm-initialized", func { BattVolts.setDoubleValue(0); init_switches(); settimer(update_electrical,5); print("Electrical System ... ok"); }); init_switches = func() { var tprop=props.globals.getNode("controls/electric/ammeter-switch",1); tprop.setBoolValue(1); tprop=props.globals.getNode("controls/lighting/instrument-lights",1); tprop.setBoolValue(0); setprop("controls/lighting/instrument-lights-norm",0.8); setprop("controls/lighting/instruments-norm",0.8); append(switch_list,"controls/engines/engine/starter"); append(output_list,"starter"); append(watt_list,10.0); append(switch_list,"controls/anti-ice/pitot-heat"); append(output_list,"pitot-heat"); append(watt_list,0.5); append(switch_list,"controls/lighting/landing-lights"); append(output_list,"landing-lights"); append(watt_list,1.0); # append(switch_list,"controls/lighting/instrument-lights"); # append(output_list,"instrument-lights"); # append(watt_list,0.2); append(switch_list,"controls/lighting/beacon-state/state"); append(output_list,"beacon"); append(watt_list,0.5); append(switch_list,"controls/lighting/nav-lights"); append(output_list,"nav-lights"); append(watt_list,0.5); append(switch_list,"controls/lighting/strobe-state/state"); append(output_list,"strobe"); append(watt_list,0.5); append(switch_list,"controls/engines/engine/fuel-pump"); append(output_list,"fuel-pump"); append(watt_list,0.5); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"adf"); append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"dme"); append(watt_list,0.2); # append(switch_list,"controls/electric/avionics-switch"); # append(output_list,"gps"); # append(watt_list,0.5); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"DG"); append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"transponder"); append(watt_list,0.2); # append(switch_list,"controls/electric/avionics-switch"); # append(output_list,"mk-viii"); # append(watt_list,0.2); # append(switch_list,"controls/electric/avionics-switch"); # append(output_list,"tacan"); # append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"turn-coordinator"); append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"comm[0]"); append(watt_list,0.2); # append(switch_list,"controls/electric/avionics-switch"); # append(output_list,"comm[1]"); # append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"nav[0]"); append(watt_list,0.2); # append(switch_list,"controls/electric/avionics-switch"); # append(output_list,"nav[1]"); # append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"autopilot"); append(watt_list,0.2); append(switch_list,"controls/electric/avionics-switch"); append(output_list,"kns80"); append(watt_list,0.2); for(var i=0; i bus_volts) { bus_volts = alternator1_volts; power_source = "alternator1"; } if (alternator2_volts > bus_volts) { bus_volts = alternator2_volts; power_source = "alternator2"; } if ( EXT.getBoolValue() and ( external_volts > bus_volts) ) { bus_volts = external_volts; } bus_volts *=PWR; load += electrical_bus(bus_volts); ammeter = 0.0; if ( power_source == "battery" ) { ammeter = -load; } else { ammeter = battery.charge_amps; } if ( power_source == "battery" ) { battery.apply_load( load, dt ); } elsif ( bus_volts > battery_volts ) { battery.apply_load( -battery.charge_amps, dt ); } ammeter_ave = 0.8 * ammeter_ave + 0.2 * ammeter; Amps.setValue(ammeter_ave); Volts.setValue(bus_volts); alternator1.apply_load(load); alternator2.apply_load(load); return load; } electrical_bus = func(bv) { var bus_volts = bv; var load = 0.0; var srvc = 0.0; for(var i=0; i