New Flight Model

package.json

@@ -1,6 +1,6 @@
 {
     "name": "salty-747",
-    "version": "0.4.0",
+    "version": "0.5.0",
     "description": "An open-source modification for the default MSFS 747-8, aiming to improve the lacking features and realism of the default aircraft.",
     "scripts": {
         "build:layout": "node scripts/build.js",

salty-747/SimObjects/Airplanes/Salty_B747_8i/ai.cfg

@@ -13,7 +13,7 @@ flareAngle = 0
 
 [STICKANDRUDDER]
 rudderGroundPID = 	0.035, 0.001, 0.1, 1.0, 1.0 ; Pk,Ik,Dk,I boundary, D boundary
-throttleGroundPID = 1.0,0.10,10.0,10.0,20.0
+throttleGroundPID = 10.0, 0.0, 0.0, 10.0, 20.0
 brakeDifferentialPID = 2.7, 0.001,10.0,1.0, 5.0
 throttleDifferentialPID = 12.0 ,0.001,25.0,10.0,40.0
 throttlePID = 50.0, 1.0, 200.0, 20.0, 500.0

salty-747/SimObjects/Airplanes/Salty_B747_8i/cameras.cfg

@@ -3,7 +3,7 @@ major =1
 minor =0
 
 [VIEWS]
-eyepoint = -18.55, -2, 11 ; (feet) longitudinal, lateral, vertical distance from reference datum
+eyepoint = -41.69, -2, 11 ; -18.55, -2, 11 ; (feet) longitudinal, lateral, vertical distance from reference datum
 
 ;===================== CAMERADEFINITION =====================
 

salty-747/SimObjects/Airplanes/Salty_B747_8i/engines.cfg

@@ -4,37 +4,46 @@ minor = 0
 
 [GENERALENGINEDATA]
 engine_type = 1 ; 0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
-fuel_flow_scalar = 1.44 ; Fuel flow scalar
+fuel_flow_scalar = 1 ; 0.8 ; Fuel flow scalar
 min_throttle_limit = -0.25 ; Minimum percent throttle.  Generally negative for turbine reverser
 master_ignition_switch = 0
 starter_type = 2 ; 0=Electric, 1=Manual, 2=Bleed Air
 max_contrail_temperature = -39.724
-Engine.0 = -119, -69.6, -7.1
+Engine.0 = -142.5, -69.95, -4.5 ; -97.5, 0, 0 ;  -119, -69.6, -7.1
 ThrustAnglesPitchHeading.0 = 0, 0
-Engine.1 = -92, -39.4, -7.5
+Engine.1 = -117, -39.35, -6.8 ; -97.5, 0, 0 ; -92, -39.4, -7.5
 ThrustAnglesPitchHeading.1 = 0, 0
-Engine.2 = -92, 39.4, -7.5
+Engine.2 = -117, 39.35, -6.8 ; -97.5, 0, 0 ; -92, 39.4, -7.5
 ThrustAnglesPitchHeading.2 = 0, 0
-Engine.3 = -119, 69.6, -7.1
+Engine.3 = -142.5, 69.95, -4.5 ; -97.5, 0, 0 ; -119, 69.6, -7.1
 ThrustAnglesPitchHeading.3 = 0, 0
 
 [TURBINEENGINEDATA]
-fuel_flow_gain = 0.002 ; Gain on fuel flow
+use_old_fuelflow_simvar = 0
+use_corrected_N2_from_FF_table = 1
+use_commanded_Ne_table = 1
+use_n2_to_n1_table = 1
+fuel_flow_gain = 1 ; 0.002 ; Gain on fuel flow
 inlet_area = 60 ; Square Feet, engine nacelle inlet area
-rated_N2_rpm = 29920 ; RPM, second stage compressor rated value
-static_thrust = 66500 ; Lbs, max rated static thrust at Sea Level
-reverser_available = 2.0
+rated_N2_rpm = 11377 ; 29920 ; RPM, second stage compressor rated value
+static_thrust = 67400 ; 66500 ; Lbs, max rated static thrust at Sea Level
+reverser_available = 1.0 ; 2.0
 reverser_mach_controlled = 0
 afterburner_available = 0
 afterburner_throttle_threshold = 0.011
-ThrustSpecificFuelConsumption = 0.24
+ThrustSpecificFuelConsumption = 0.27
 AfterBurnThrustSpecificFuelConsumption = 0.011
-mach_0_corrected_commanded_ne_table = 0.000000:1.000000:22.570000,0.000000:55.000000:82.500000,0.420000:78.800003:95.400002,0.510000:82.500000:98.500000,0.610000:87.400002:101.099998,0.700000:92.000000:103.099998,0.790000:96.199997:105.699997,0.930000:103.099998:108.059998,1.000000:107.000000:108.059998
-mach_hi_corrected_commanded_ne_table = 0.900000:1.000000:22.570000,0.000000:62.000000:82.500000,0.420000:77.000000:95.400002,0.510000:80.199997:98.500000,0.610000:84.800003:101.099998,0.700000:89.099998:103.099998,0.790000:92.199997:105.699997,0.930000:96.000000:108.059998,1.000000:98.199997:108.059998
-corrected_n2_from_ff_table = 0.000000:0.000000, 0.002940:10.000000, 0.011800:30.000000, 0.020660:40.000000, 0.033970:50.000000, 0.053170:60.000000, 0.133910:80.000000, 0.257710:90.000000, 0.540000:100.000000, 0.686860:108.000000
-n1_and_mach_on_thrust_table = 0.000000:0.000000:0.900000,0.000000:0.000000:0.000000,20.000000:0.025400:0.114000,25.000000:0.050800:0.222000,30.000000:0.079800:0.350000,35.000000:0.112500:0.451000,40.000000:0.152400:0.545000,45.000000:0.199500:0.640000,50.000000:0.254000:0.754000,55.000000:0.360000:0.869000,60.000000:0.480000:0.953000,65.000000:0.572000:1.040000,70.000000:0.653000:1.126000,75.000000:0.727000:1.210000,80.000000:0.788000:1.295000,85.000000:0.875000:1.378000,90.000000:0.985000:1.478000,95.000000:1.061000:1.578000,100.000000:1.153000:1.668000,105.000000:1.237000:1.778000,110.000000:1.338000:1.845000
-n2_to_n1_table = 0.000000:0.000000:0.900000,0.000000:0.000000:0.000000,10.000000:1.100000:1.000000,20.000000:2.700000:2.400000,30.000000:5.700000:4.700000,40.000000:10.100000:8.400000,50.000000:17.500000:12.800000,60.000000:29.900000:21.200001,70.000000:49.400002:41.599998,80.000000:67.500000:60.400002,90.000000:90.599998:85.900002,100.000000:105.500000:102.400002,110.000000:118.000000:114.099998
-corrected_airflow_table = 0.000000:0.000000:0.900000,0.000000:0.000000:0.000000,20.000000:4.290000:14.081000,85.000000:22.000000:24.000000,90.000000:25.000000:25.000000,95.000000:27.000000:27.000000,100.000000:28.000000:28.000000,105.000000:29.000000:29.000000,110.000000:30.000000:30.000000
+mach_0_corrected_commanded_ne_table = 0.000:1.000:1.202:1.454:2.178:3.367:4.250:5.403:6.870,0.000:68.00:69.21:70.49:73.28:76.42:78.15:78.42:78.42,0.143:74.20:75.52:76.91:79.95:83.39:85.27:85.57:85.57,0.286:80.40:81.83:83.34:86.63:90.35:92.40:92.72:92.72,0.429:86.59:88.14:89.76:93.31:97.32:99.52:99.86:99.86,0.572:92.79:94.44:96.19:99.99:104.28:106.64:107.01:107.01,0.715:98.99:100.75:102.61:106.67:111.25:113.77:114.16:114.16,0.858:105.19:107.06:109.04:113.35:118.21:120.89:121.31:121.31,1.000:111.34:113.32:115.42:119.98:125.13:127.96:128.40:128.40
+mach_hi_corrected_commanded_ne_table = 1.000:1.000:1.202:1.454:2.178:3.367:4.250:5.403:6.870,0.000:62.08:63.18:64.35:66.89:69.76:71.34:71.59:71.59,0.143:67.73:68.94:70.21:72.99:76.12:77.85:78.11:78.11,0.286:73.39:74.70:76.08:79.08:82.48:84.35:84.64:84.64,0.429:79.05:80.46:81.94:85.18:88.84:90.85:91.16:91.16,0.572:84.71:86.21:87.81:91.28:95.19:97.35:97.69:97.69,0.715:90.36:91.97:93.67:97.37:101.55:103.85:104.21:104.21,0.858:96.02:97.73:99.54:103.47:107.91:110.36:110.74:110.74,1.000:101.64:103.45:105.36:109.52:114.22:116.81:117.22:117.22
+corrected_n2_from_ff_table = 0.0:0.0,0.0020789:25,0.0241155:68,0.0270274:70,0.0477917:80,0.0845086:90,0.1494337:100,0.2642387:110,0.4672446:120
+;n1_and_mach_on_thrust_table = 0:0:0.1:0.2:0.3:0.4:0.5:0.6:0.7:0.8:0.9:1,0:0:0:0:0:0:0:0:0:0:0:0,20.2:0.0407:0.0361:0.0319:0.0281:0.0248:0.0219:0.0196:0.0177:0.0165:0.0159:0.0161,30.0:0.0610:0.0541:0.0478:0.0421:0.0371:0.0328:0.0293:0.0265:0.0247:0.0238:0.0241,40.0:0.0920:0.0816:0.0721:0.0636:0.0560:0.0496:0.0442:0.0401:0.0373:0.0360:0.0363,50.0:0.1390:0.1232:0.1089:0.0960:0.0846:0.0748:0.0667:0.0605:0.0563:0.0544:0.0549,60.0:0.2098:0.1861:0.1644:0.1450:0.1278:0.1130:0.1008:0.0914:0.0850:0.0821:0.0828,70.0:0.3168:0.2809:0.2482:0.2189:0.1929:0.1706:0.1522:0.1380:0.1284:0.1239:0.1251,80.0:0.4783:0.4241:0.3748:0.3304:0.2912:0.2575:0.2297:0.2083:0.1939:0.1871:0.1889,90.0:0.7222:0.6404:0.5659:0.4989:0.4397:0.3888:0.3468:0.3145:0.2927:0.2825:0.2852,97.9:1.0000:0.8867:0.7836:0.6908:0.6089:0.5384:0.4803:0.4355:0.4053:0.3912:0.3948,100.0:1.0904:0.9669:0.8544:0.7533:0.6639:0.5871:0.5237:0.4748:0.4419:0.4265:0.4305,120.0:2.4856:2.2041:1.9477:1.7171:1.5135:1.3383:1.1938:1.0824:1.0074:0.9723:0.9814
+n1_and_mach_on_thrust_table = 0.00:0.00:0.10:0.20:0.30:0.40:0.50:0.60:0.70:0.80:0.90:1.00,0.00:0.00:0.00:0.00:0.00:0.00:0.00:0.00:0.00:0.00:0.00:0.00,20.2:0.0409:0.0370:0.0335:0.0305:0.0279:0.0258:0.0241:0.0230:0.0225:0.0227:0.0236,40.0:0.0919:0.0832:0.0754:0.0685:0.0627:0.0579:0.0542:0.0518:0.0507:0.0511:0.0531,50.0:0.1384:0.1252:0.1135:0.1032:0.0943:0.0871:0.0816:0.0779:0.0763:0.0769:0.0799,60.0:0.2083:0.1885:0.1708:0.1553:0.1420:0.1311:0.1228:0.1173:0.1148:0.1157:0.1203,70.0:0.3135:0.2837:0.2571:0.2337:0.2138:0.1974:0.1849:0.1766:0.1729:0.1742:0.1810,80.0:0.4719:0.4271:0.3870:0.3519:0.3218:0.2972:0.2784:0.2658:0.2602:0.2622:0.2725,90.0:0.7104:0.6429:0.5826:0.5297:0.4844:0.4473:0.4190:0.4002:0.3917:0.3946:0.4102,95.0:0.8716:0.7888:0.7148:0.6499:0.5944:0.5489:0.5141:0.4910:0.4806:0.4842:0.5033,97.9:0.9813:0.8881:0.8048:0.7317:0.6692:0.6180:0.5788:0.5528:0.5411:0.5451:0.5667,98.5:1.0057:0.9102:0.8248:0.7499:0.6858:0.6333:0.5932:0.5665:0.5545:0.5587:0.5807,99.0:1.0257:0.9282:0.8412:0.7647:0.6994:0.6459:0.6050:0.5777:0.5655:0.5698:0.5923,100.0:1.0693:0.9678:0.8770:0.7973:0.7292:0.6734:0.6307:0.6024:0.5896:0.5940:0.6175,105.0:1.3120:1.1874:1.0760:0.9782:0.8947:0.8262:0.7739:0.7390:0.7234:0.7288:0.7576,110.0:1.6097:1.4568:1.3201:1.2002:1.0977:1.0137:0.9495:0.9067:0.8875:0.8942:0.9295,120.0:2.4231:2.1929:1.9872:1.8067:1.6524:1.5259:1.4292:1.3649:1.3360:1.3461:1.3992
+;n2_to_n1_table = 0.0:0.0:1.0,0.0:0.0:0.0,10.0:0.7:0.7,20.0:2.2:2.2,30.0:4.4:4.4,40.0:7.5:7.5,50.0:11.3:11.3,60.0:15.9:15.9,68.0:20.2:20.2,80.0:41.9:41.9,90.0:59.9:59.9,100.0:78.0:78.0,120.0:114.1:114.1
+;n2_to_n1_table = 0.0:0.0:1.0,0.0:0.00:0.00,10.0:0.70:0.70,20.0:2.18:2.18,30.0:4.44:4.44,40.0:7.48:7.48,50.0:11.30:11.30,60.0:15.89:15.90,68.0:20.20:20.20,80.0:41.88:41.89,90.0:59.94:59.96,100.0:78.01:78.03,120.0:114.14:123.98
+n2_to_n1_table = 0.0:0.0:1.0,0.0:0.00:0.00,10.0:0.70:0.77,20.0:2.18:2.39,30.0:4.44:4.86,40.0:7.48:8.19,50.0:11.30:12.37,60.0:15.89:17.41,68.0:20.20:22.13,80.0:41.88:45.88,90.0:59.94:65.67,100.0:78.01:85.46,120.0:114.14:125.04
+;corrected_airflow_table = 0.00:0.00:1.00,0.00:0.00:0.00,20.2:1.58:0.92,40.0:3.89:2.25,50.0:5.11:2.96,60.0:7.89:4.57,70.0:13.17:7.62,80.0:21.74:12.58,90.0:32.35:18.72,97.9:38.28:22.15,98.5:38.80:22.45,100.0:39.43:22.82,110.0:41.16:23.82
+;corrected_airflow_table = 0.000000:0.000000:0.900000,0.000000:0.000000:0.000000,20.000000:4.290000:14.081000,85.000000:22.000000:24.000000,90.000000:25.000000:25.000000,95.000000:27.000000:27.000000,100.000000:28.000000:28.000000,105.000000:29.000000:29.000000,110.000000:30.000000:30.000000
+;jet_density_on_ff_table = 0.000460:0.3522, 0.000585:0.3847, 0.000737:0.4131, 0.000890:0.4695, 0.001066:0.5505, 0.001267:0.6420, 0.001496:0.7532, 0.001756:0.7786, 0.002049:0.8956, 0.002378:1.0
 epr_max = 1.4
 epr_tc = 14
 epr_tuning_constant = 1
@@ -45,14 +54,15 @@ oil_temp_tuning_constant = 1
 oil_press_max = 12384
 oil_press_tc = 0.8
 oil_press_tuning_constant = 1
-fuel_flow_max_itt_factor = 2.0
-fuel_flow_min_itt_factor = 0.72
-n1_cooling_factor = 0.01
-itt_peak_temperature = 2141
-itt_tc = 2
+fuel_flow_max_itt_factor = 1.5 ; 2.0
+fuel_flow_min_itt_factor = 0.67 ; 0.72
+n1_cooling_factor = 0 ; 0.01
+itt_peak_temperature = 3012 ; 2141
+itt_tc = 2 ; 2
 itt_tuning_constant = 1
-egt_peak_temperature = 1600
-egt_tc = 2
+itt_cooling_factor = 0.01
+egt_peak_temperature = 1917 ; 1600
+egt_tc = 2 ; 2
 egt_tuning_constant = 1
 fuel_press_max = 2376
 fuel_press_tc = 2
@@ -61,46 +71,47 @@ variable_inlet = 0
 primary_nozzle_available = 0
 primary_nozzle_afterburner_offset = 0.14
 primary_nozzle_n1_mach_to_nozzle_pos = 0.000000:0.000000:2.000000,53.000000:0.660000:0.100000,65.000000:0.690000:0.330000,96.000000:0.700000:0.440000
-density_on_torque_table = 0.000225:0.100000, 0.000352:0.300000, 0.000480:0.500000, 0.000607:0.700000, 0.000734:0.900000, 0.000862:1.000000, 0.001241:1.000000, 0.001620:1.000000, 0.001999:1.000000, 0.002378:1.000000
+;density_on_torque_table = 0.000225:0.100000, 0.000352:0.300000, 0.000480:0.500000, 0.000607:0.700000, 0.000734:0.900000, 0.000862:1.000000, 0.001241:1.000000, 0.001620:1.000000, 0.001999:1.000000, 0.002378:1.000000
 starter_N1_max_pct = 12 ; Pct, percentage of max rpm that reached using only starter.
 starter_N1_rate = 12 ; Rate at which the starter N1 increases.
-ignition_auto_type = "Starter,Flaps,AntiIce" ; If the Ignition is set to AUTO - specifies how that is handled. 0(default) = Always on, 1 = Ignition follows starter status, 2 = Ignition enabled when Flaps are not neutral, when AntiIce is enabled, or when N1/N2 is below 50%.
-min_condition_lever_for_combustion = 0.01 ; % - Minimum position of the Condition lever to obtain a combustion. Default at 0.01.
-min_n1_for_combustion = 10 ; % - Minimum N1 required to maintain a combustion
+ignition_auto_type = "Starter,Flaps,AntiIce,N2" ; If the Ignition is set to AUTO - specifies how that is handled. 0(default) = Always on, 1 = Ignition follows starter status, 2 = Ignition enabled when Flaps are not neutral, when AntiIce is enabled, or when N1/N2 is below 50%.
+min_condition_lever_for_combustion = 0 ; 0.01 ; % - Minimum position of the Condition lever to obtain a combustion. Default at 0.01.
+min_n1_for_combustion = 10.0 ; % - Minimum N1 required to maintain a combustion
 min_n2_for_combustion = 19.4 ; % - Minimum N2 required to maintain a combustion
 min_n1_for_starter_cutoff = 200 ; % - Minimum N1 at which the starter is automatically disabled
-min_n2_for_starter_cutoff = 50 ; % - Minimum N2 at which the starter is automatically disabled
+min_n2_for_starter_cutoff = 200 ; 50 ; % - Minimum N2 at which the starter is automatically disabled
 min_n2_for_apu_bleed_air_cutoff = 200 ; % - Minimum N2 at which the APU Bleed Air is automatically disabled
-n2_from_bleed_air_psi_table = 0:0, 4:8, 10:18, 18:25 ; Table which contains the n2 generated depending on the pression from the bleed air from the APU (in psi).
+n2_from_bleed_air_psi_table = 0:0, 4:8, 10:18, 18:30 ; Table which contains the n2 generated depending on the pression from the bleed air from the APU (in psi).
 bleed_air_on_n2_tc = 1 ; Time constant which contains the speed at which the bleed air pressure affect the N2 of the turbine.
 N1_to_oil_pressure_table = 0:0, 0.21:0.88, 0.9:0.954, 1:1 ; % of max Oil Pressure for % N1.
-n1_normal_tc = 0.5 ; Float factor changing N1 acceleration during normal use of the engine
+n1_normal_tc = 0.25 ; 0.5 ; Float factor changing N1 acceleration during normal use of the engine
 n1_start_max_rate = 1.0 ; Float limiting N1 acceleration during starter use
 n1_start_combustion_max_rate = 2.0 ; Float limiting N1 acceleration during startup when cumbustion has started
-idle_fuel_flow = 1364 ; pound per hour
-low_idle_n1 = 23.2
-low_idle_n2 = 60
-high_n1 = 98
-high_n2 = 102
-high_fuel_flow = 8000
-min_n2_for_fuel_flow = 22
-mach_influence_on_n1 = 10
-fuel_flow_max = 10000
-fuel_flow_controller_p = 0.5
-fuel_flow_controller_i = 0.1
-fuel_flow_controller_d = 0.5
+idle_fuel_flow = 1714 ; 3100 ; pound per hour
+low_idle_n1 = 20.2 ; 23.2
+low_idle_n2 = 68 ; 60
+high_n1 = 106.7 ; 106.7 ; 98 ; 106.7 ; 100 ; 98
+high_n2 = 118.0 ; 118.0 ; 102 ; 118.0 ; 100 ; 102
+high_fuel_flow = 50000 ; 8000
+min_n2_for_fuel_flow = 25 ; 22
+mach_influence_on_n1 = 0
+fuel_flow_max = 50000 ; 25000 ; 10000
+fuel_flow_controller_p = 1.0 ; 0.8 ; 0.5
+fuel_flow_controller_i = 0.01 ; 0.1
+fuel_flow_controller_d = 0.0 ; 0.5
 fuel_flow_controller_iboundary = 5
 fuel_flow_controller_dboundary = 100
 max_torque_protection = 0 ; 0 = no protection, value of the torque triggering a protection by automatically limiting the fuelflow
-max_n1_protection = 104 ; 0 = no protection, value of the n1 triggering a protection by automatically limiting the fuelflow
-max_n2_protection = 105 ; 0 = no protection, value of the n2 triggering a protection by automatically limiting the fuelflow
-max_egt_protection = 2000 ; 0 = no protection, value of the egt triggering a protection by automatically limiting the fuelflow
+max_n1_protection = 0 ; 106.7 ; 104 ; 0 = no protection, value of the n1 triggering a protection by automatically limiting the fuelflow
+max_n2_protection = 0 ; 118.0 ; 105 ; 0 = no protection, value of the n2 triggering a protection by automatically limiting the fuelflow
+max_egt_protection = 0 ; 2408.67 ; 2000 ; 0 = no protection, value of the egt triggering a protection by automatically limiting the fuelflow
 
 [JET_ENGINE]
-thrust_scalar = 0.85
+thrust_scalar = 1 ; 0.85
 
 [DISABLED_CONTROLS]
-DisableFuelValveControls = 0 ; Disable fuel valve controls
+DisableFuelValveControls = 1 ; Disable fuel valve controls
 DisableMixtureControls = 1 ; Disable mixture controls
 DisableParkingBrakeControls = 0 ; Disable parking brake controls
 DisablePropellerControls = 1 ; Disable propeller controls
+