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fix(a380x/flightmodel): adjust climb performance #9358

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merged 18 commits into from
Dec 28, 2024
Merged

fix(a380x/flightmodel): adjust climb performance #9358

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e01598b
Adjust climb performance
BlueberryKing Nov 3, 2024
4c9441d
Tune to drag coefficient 1
BlueberryKing Nov 5, 2024
dacb4b8
Adjust REC MAX altitude
BlueberryKing Nov 6, 2024
1c0103e
Make engine performance table aircraft-specific
BlueberryKing Nov 7, 2024
ed38c3e
Fix incorrect arguments being passed
BlueberryKing Nov 9, 2024
5112652
Try adjusting to in-sim tests
BlueberryKing Nov 9, 2024
20113fb
Merge with taxi thrust adjustment
BlueberryKing Nov 10, 2024
b761498
Add changelog
BlueberryKing Nov 10, 2024
b8d971e
Make flight model aircraft-specific
BlueberryKing Nov 10, 2024
01da2f9
Fix typo
BlueberryKing Nov 12, 2024
2589740
Add changelog
BlueberryKing Nov 10, 2024
4e6835d
Fix changelog
BlueberryKing Nov 15, 2024
ec19552
Increase thrust limits
BlueberryKing Nov 24, 2024
0457889
Increase high-mach thrust
BlueberryKing Nov 24, 2024
244a09f
Separate thrust limit between aircraft
BlueberryKing Nov 24, 2024
dffb850
Increase thrust limits around FL300
BlueberryKing Nov 27, 2024
1aa931e
Increase high-mach thrust after feedback
BlueberryKing Nov 27, 2024
163cbb6
Increase thrust
BlueberryKing Dec 21, 2024
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5 changes: 5 additions & 0 deletions .github/CHANGELOG.md
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Original file line number Diff line number Diff line change
Expand Up @@ -37,6 +37,8 @@
1. [A380X/FUEL] Recalibrated inital fuel settings - @sschiphorst (Yahtzee94)
1. [A380X/ENG] Another adjustment to taxi thrust - @donstim (donbikes)
1. [A380X/ANIM] Animation of flaps now from FPPU position. Interim fix for spoiler low end animation - @Crocket63 (crocket)
1. [A380X/ENGINES] Another adjustment to taxi thrust - @donstim (donbikes)
1. [A380/ANIM] Animation of flaps now from FPPU position. Interim fix for spoiler low end animation - @Crocket63 (crocket)
1. [A380X/ENG] Improve oil pressure lookup table - @tracernz (Mike)
1. [A380X/FADEC] Add N1 fan protection measures (METOTS, KOZ) - @flogross89 (floridude)
1. [A380/WING_FLEX] Reduced stiffness of wings for more tip up bend - @Crocket63 (crocket)
Expand Down Expand Up @@ -98,6 +100,9 @@
1. [ELEC] Improved elec system startup behaviour - @Gurgel100 (Pascal) - @saschl
1. [A380X] Improve pilot and copilot camera positions - @heclak (Heclak)
1. [A380X/EFIS] Illuminate ND range and mode selectors during light test - @BravoMike99 (bruno_pt99)
1. [A380X/ENG] Adjust climb thrust to be more accurate - @BlueberryKing (BlueberryKing)
1. [A380X/ANIM] Animation of flaps now from FPPU position. Interim fix for spoiler low end animation - @Crocket63 (crocket)
2hwk marked this conversation as resolved.
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1. [A380X/ENGINES] Adjust climb thrust to be more accurate - @BlueberryKing (BlueberryKing)

## 0.12.0

Expand Down
104 changes: 102 additions & 2 deletions fbw-a32nx/src/systems/fmgc/src/flightplanning/A320AircraftConfig.ts
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Original file line number Diff line number Diff line change
Expand Up @@ -11,6 +11,7 @@ import {
VnavConfig,
VnavDescentMode,
} from '@fmgc/flightplanning/AircraftConfigTypes';
import { FlapConf } from '@fmgc/guidance/vnav/common';

const lnavConfig: LnavConfig = {
DEFAULT_MIN_PREDICTED_TAS: 160,
Expand All @@ -25,7 +26,7 @@ const vnavConfig: VnavConfig = {
DEBUG_GUIDANCE: false,
ALLOW_DEBUG_PARAMETER_INJECTION: false,
VNAV_USE_LATCHED_DESCENT_MODE: false,
IDLE_N1_MARGIN: 3,
IDLE_N1_MARGIN: 2,
MAXIMUM_FUEL_ESTIMATE: 40000,
};

Expand All @@ -42,13 +43,112 @@ const flightModelParams: FlightModelParameters = {
dragCoefficientCorrections: [0, 0.0002, 0.0003, 0.0004, 0.0008, 0.0015, 0.01],
speedBrakeDrag: 0.01008,
gearDrag: 0.0372,
dragCoeffFactor: 1,
dragPolarCoefficients: {
[FlapConf.CLEAN]: [0.0215, -0.015, 0.0412, 0.0211],
[FlapConf.CONF_1]: [0.0398, -0.0538, 0.1166, -0.064, 0.0303],
[FlapConf.CONF_2]: [0.0729, -0.0037, -0.0018, 0.0168],
[FlapConf.CONF_3]: [0.0902, 0.0005, -0.0056, 0.013],
[FlapConf.CONF_FULL]: [0.1405, -0.001, -0.0056, 0.0077],
},
};

const engineModelParams: EngineModelParameters = {
maxThrust: 27120,
numberOfEngines: 2,
fuelBurnFactor: 1.0,
cn1ClimbLimit: [
[0, 2000, 5000, 8000, 12000, 15000, 17000, 20000, 24000, 27000, 31000, 35000, 39000, 41500],
[-54.0, 71.8, 73.6, 75.5, 76.8, 78.1, 78.9, 80.1, 81.5, 81.6, 83.0, 83.6, 83.7, 83.3],
[-50.0, 72.5, 74.3, 76.2, 77.5, 78.8, 79.6, 80.9, 82.2, 82.4, 83.8, 84.4, 84.5, 84.0],
[-46.0, 73.1, 75.0, 76.9, 78.2, 79.5, 80.3, 81.6, 83.0, 83.1, 84.5, 85.1, 85.3, 84.8],
[-42.0, 73.8, 75.6, 77.6, 78.9, 80.2, 81.0, 82.3, 83.7, 83.8, 85.3, 85.9, 86.0, 85.5],
[-38.0, 74.4, 76.3, 78.2, 79.6, 80.9, 81.7, 83.0, 84.4, 84.6, 86.0, 86.6, 86.7, 86.3],
[-34.0, 75.0, 76.9, 78.9, 80.3, 81.6, 82.4, 83.7, 85.1, 85.3, 86.7, 87.3, 87.5, 87.0],
[-30.0, 75.7, 77.6, 79.6, 80.9, 82.2, 83.1, 84.4, 85.8, 86.0, 87.5, 88.1, 88.2, 87.7],
[-26.0, 76.3, 78.2, 80.2, 81.6, 82.9, 83.8, 85.1, 86.5, 86.7, 88.2, 88.8, 88.9, 88.4],
[-22.0, 76.9, 78.8, 80.9, 82.2, 83.6, 84.4, 85.8, 87.2, 87.4, 88.9, 89.5, 89.6, 89.1],
[-18.0, 77.5, 79.5, 81.5, 82.9, 84.2, 85.1, 86.5, 87.9, 88.1, 89.6, 90.2, 90.0, 89.5],
[-14.0, 78.1, 80.1, 82.1, 83.5, 84.9, 85.8, 87.1, 88.6, 88.8, 90.3, 90.0, 89.2, 88.7],
[-10.0, 78.7, 80.7, 82.8, 84.2, 85.6, 86.4, 87.8, 89.3, 89.5, 91.0, 89.2, 88.4, 87.9],
[-6.0, 79.3, 81.3, 83.4, 84.8, 86.2, 87.1, 88.5, 90.0, 90.1, 91.1, 88.5, 87.7, 87.1],
[-2.0, 79.9, 81.9, 84.0, 85.5, 86.8, 87.7, 89.1, 90.6, 90.8, 90.2, 87.7, 86.9, 86.4],
[2.0, 80.5, 82.5, 84.6, 86.1, 87.5, 88.4, 89.8, 91.3, 90.3, 89.5, 87.0, 86.2, 85.6],
[6.0, 81.1, 83.1, 85.3, 86.7, 88.1, 89.0, 90.4, 90.5, 89.5, 88.8, 86.3, 85.5, 84.9],
[10.0, 81.6, 83.7, 85.9, 87.3, 88.7, 89.7, 90.0, 89.6, 88.7, 88.1, 85.6, 84.8, 84.2],
[14.0, 82.2, 84.3, 86.5, 87.9, 89.4, 89.3, 89.1, 88.7, 87.9, 87.5, 84.8, 83.9, 83.3],
[18.0, 82.8, 84.9, 87.1, 88.5, 88.6, 88.4, 88.3, 87.9, 87.2, 86.8, 86.8, 86.8, 86.8],
[22.0, 83.4, 85.5, 86.9, 88.0, 87.8, 87.7, 87.5, 87.2, 86.5, 86.1, 86.1, 86.1, 86.1],
[26.0, 83.9, 85.7, 86.2, 87.2, 87.1, 87.0, 86.8, 86.5, 85.8, 85.4, 85.4, 85.4, 85.4],
[30.0, 84.5, 84.9, 85.4, 86.5, 86.4, 86.3, 86.1, 85.8, 85.1, 85.1, 85.1, 85.1, 85.1],
[34.0, 83.8, 84.2, 84.7, 85.8, 85.7, 85.6, 85.5, 85.1, 85.1, 85.1, 85.1, 85.1, 85.1],
[38.0, 83.0, 83.4, 83.9, 85.1, 85.0, 84.9, 84.8, 84.8, 84.8, 84.8, 84.8, 84.8, 84.8],
[42.0, 82.2, 82.6, 83.1, 84.4, 84.4, 84.3, 84.3, 84.3, 84.3, 84.3, 84.3, 84.3, 84.3],
[46.0, 81.4, 81.8, 82.4, 83.7, 83.7, 83.7, 83.7, 83.7, 83.7, 83.7, 83.7, 83.7, 83.7],
[50.0, 80.6, 81.1, 81.6, 83.0, 83.0, 83.0, 83.0, 83.0, 83.0, 83.0, 83.0, 83.0, 83.0],
[54.0, 79.9, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4, 80.4],
[58.0, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2, 79.2],
],
table1502: [
[0, 0, 0.2, 0.9],
[18.2, 0.0, 0.0, 17.0],
[22.0, 1.9, 1.9, 17.4],
[26.0, 2.5, 2.5, 18.2],
[57.0, 12.8, 12.8, 27.0],
[68.2, 19.6, 19.6, 34.827774],
[77.0, 26.0, 26.0, 40.839552],
[83.0, 31.42024, 31.42024, 44.768766],
[89.0, 40.972041, 40.972041, 50.09214],
[92.8, 51.0, 51.0, 55.042],
[97.0, 65.0, 65.0, 65.0],
[100.0, 77.0, 77.0, 77.0],
[104.0, 85.0, 85.0, 85.5],
[116.5, 101.0, 101.0, 101.0],
],
table1503: [
[0, 1.0, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313],
[0.0, 68.2, 69.402657, 70.671269, 73.432244, 76.544349, 78.644882, 78.644882],
[0.1, 76.0, 77.340205, 78.753906, 81.830654, 85.298688, 87.639458, 87.639458],
[0.2, 83.0, 84.463645, 86.007556, 89.367688, 93.155146, 95.711513, 95.711513],
[0.4, 92.8, 94.436461, 96.162664, 99.919535, 104.154188, 107.01239, 107.01239],
[0.6, 98.0, 99.728159, 101.55109, 105.518475, 109.990414, 113.008774, 113.008774],
[0.75, 101.5, 103.289879, 105.177914, 109.286991, 113.918643, 117.044802, 117.044802],
[0.9, 103.0, 104.81633, 106.0, 110.90207, 115.60217, 118.774528, 118.774528],
[1.0, 104.2, 106.037491, 107.97575, 112.194133, 116.948991, 120.158309, 120.158309],
],
table1504: [
[0, 1.0, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313],
[0.0, 63.267593, 64.383271, 65.560133, 68.121427, 71.008456, 72.957073, 72.957073],
[0.1, 70.503476, 71.746753, 73.058212, 75.912441, 79.129658, 81.301137, 81.301137],
[0.2, 76.997217, 78.355007, 79.787258, 82.904376, 86.417916, 88.789399, 88.789399],
[0.4, 86.088455, 87.606562, 89.207922, 92.693086, 96.621477, 99.272967, 99.272967],
[0.6, 90.912377, 92.51555, 94.206642, 97.887095, 102.035612, 104.835676, 104.835676],
[0.75, 94.159247, 95.819677, 97.571165, 101.383063, 105.679741, 108.579808, 108.579808],
[0.9, 95.550763, 97.235732, 98.333795, 102.881334, 107.24151, 110.184435, 110.184435],
[1.0, 104.2, 106.037491, 107.97575, 112.194133, 116.948991, 120.158309, 120.158309],
],
table1506: [
[0.0, 0.0, 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9],
[0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0],
[20.0, 0.091741, 0.05702, 0.052029, 0.028096, -0.017284, -0.037284, -0.057077, -0.205841, -0.315399, -0.488717],
[25.0, 0.14281, 0.072215, 0.053026, 0.030404, -0.009593, -0.026571, -0.041999, -0.151328, -0.266204, -0.439028],
[30.0, 0.189837, 0.082322, 0.05505, 0.032748, 0.017389, 0.00399, -0.026921, -0.051814, -0.081946, -0.369391],
[35.0, 0.262207, 0.126047, 0.077206, 0.045921, 0.024719, 0.006062, -0.002812, -0.0228, -0.044248, -0.293631],
[40.0, 0.33023, 0.162757, 0.124088, 0.069579, 0.057905, 0.049621, 0.02979, -0.002139, -0.025811, -0.22063],
[45.0, 0.393293, 0.250096, 0.156707, 0.112419, 0.091418, 0.076757, 0.05609, 0.018509, -0.007375, -0.15512],
[50.0, 0.452337, 0.311066, 0.211353, 0.158174, 0.127429, 0.104915, 0.081171, 0.047419, 0.011062, -0.098474],
[55.0, 0.509468, 0.373568, 0.269961, 0.209106, 0.16865, 0.137223, 0.108383, 0.07566, 0.028704, -0.049469],
[60.0, 0.594614, 0.439955, 0.334629, 0.267477, 0.217773, 0.176899, 0.141404, 0.107148, 0.064556, -0.005036],
[65.0, 0.660035, 0.512604, 0.407151, 0.335055, 0.276928, 0.226669, 0.183627, 0.14585, 0.104441, 0.039012],
[70.0, 0.733601, 0.593506, 0.488571, 0.412623, 0.347163, 0.28821, 0.237559, 0.195142, 0.152485, 0.087269],
[75.0, 0.818693, 0.68388, 0.578756, 0.499514, 0.427939, 0.361604, 0.304241, 0.257197, 0.212005, 0.144042],
[80.0, 0.910344, 0.783795, 0.675982, 0.593166, 0.516644, 0.444822, 0.382689, 0.332384, 0.284867, 0.212679],
[85.0, 1.025165, 0.891823, 0.776548, 0.688692, 0.608128, 0.53321, 0.469351, 0.41869, 0.37087, 0.294907],
[90.0, 1.157049, 1.004695, 0.8744, 0.778466, 0.694251, 0.619011, 0.557581, 0.511153, 0.467149, 0.390203],
[95.0, 1.281333, 1.116993, 0.960774, 0.851733, 0.763455, 0.69089, 0.637136, 0.601322, 0.567588, 0.495167],
[100.0, 1.357935, 1.220844, 1.023864, 0.894234, 0.800352, 0.733488, 0.693684, 0.654691, 0.617963, 0.539115],
[105.0, 1.378826, 1.239626, 1.048498, 0.91575, 0.819609, 0.751137, 0.710375, 0.670444, 0.632832, 0.552086],
[110.0, 1.392754, 1.252148, 1.069322, 0.933937, 0.835886, 0.766054, 0.724483, 0.683759, 0.6454, 0.563051],
],
};

const fmsSymbolConfig: FMSymbolsConfig = {
Expand Down
140 changes: 137 additions & 3 deletions fbw-a32nx/src/systems/fmgc/src/flightplanning/A380AircraftConfig.ts
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Original file line number Diff line number Diff line change
Expand Up @@ -11,6 +11,7 @@ import {
VnavConfig,
VnavDescentMode,
} from '@fmgc/flightplanning/AircraftConfigTypes';
import { FlapConf } from '@fmgc/guidance/vnav/common';

const lnavConfig: LnavConfig = {
DEFAULT_MIN_PREDICTED_TAS: 160,
Expand All @@ -37,17 +38,150 @@ const flightModelParams: FlightModelParameters = {
requiredAccelRateMS2: 0.684,
gravityConstKNS: 19.0626,
gravityConstMS2: 9.806665,
machValues: [0.55, 0.6, 0.65, 0.7, 0.75, 0.8, 0.85],
dragCoefficientCorrections: [0, 0.0002, 0.0003, 0.0004, 0.0008, 0.0015, 0.01],
machValues: [0, 0.5, 0.55, 0.6, 0.65, 0.7, 0.75, 0.8, 0.85, 0.9, 0.95, 1.0],
dragCoefficientCorrections: [0, 0, 0, 0.0002, 0.0003, 0.0004, 0.0008, 0.0013, 0.002, 0.005, 0.016, 0.1],
speedBrakeDrag: 0.0201,
gearDrag: 0.00872,
dragCoeffFactor: 0.87,
dragPolarCoefficients: {
[FlapConf.CLEAN]: [0.025, -5.48e-3, -0.0192, 0.0582],
[FlapConf.CONF_1]: [0.0398, -0.0538, 0.1166, -0.064, 0.0303],
[FlapConf.CONF_2]: [0.0729, -0.0037, -0.0018, 0.0168],
[FlapConf.CONF_3]: [0.0902, 0.0005, -0.0056, 0.013],
[FlapConf.CONF_FULL]: [0.1405, -0.001, -0.0056, 0.0077],
},
};

const engineModelParams: EngineModelParameters = {
maxThrust: 80_213,
numberOfEngines: 4,
fuelBurnFactor: 1.33,
/**
* Maximum N1 in CLB thrust
* @param i row index (tat) in steps of 4°C
* @param j col index (pressure altitude, ft)
* @returns Corrected N1 (CN1)
*/
cn1ClimbLimit: [
[0, 2000, 5000, 8000, 12000, 15000, 17000, 20000, 24000, 27000, 31000, 35000, 39000, 41500],
[-54, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-50, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-46, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-42, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-38, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-34, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-30, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-26, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-22, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-18, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 102.0, 104.1, 105.5],
[-14, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 100.5, 102.5, 103.9],
[-10, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 99.1, 100.9, 102.3],
[-6, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 99.5, 97.7, 99.3, 100.6],
[-2, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 96.2, 98.1, 96.2, 97.7, 99.0],
[2, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 94.6, 94.8, 96.6, 94.8, 96.1, 97.3],
[6, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 92.1, 93.2, 93.5, 95.1, 93.3, 94.5, 95.7],
[10, 82.6, 84.6, 86.8, 88.3, 89.7, 90.7, 90.8, 91.8, 92.1, 93.7, 91.9, 92.9, 94.0],
[14, 82.6, 84.6, 86.8, 88.3, 89.7, 89.4, 89.6, 90.4, 90.8, 92.2, 90.5, 91.3, 92.4],
[18, 82.6, 84.6, 86.8, 88.3, 88.5, 88.2, 88.3, 89.1, 89.4, 90.7, 89.0, 89.7, 90.7],
[22, 82.6, 84.6, 85.6, 87.1, 87.3, 87.0, 87.0, 87.7, 88.1, 89.2, 87.6, 88.1, 89.1],
[26, 82.6, 84.6, 84.5, 85.9, 86.0, 85.8, 85.7, 86.3, 86.7, 87.8, 86.1, 86.5, 87.4],
[30, 82.6, 83.4, 83.3, 84.7, 84.8, 84.6, 84.4, 84.9, 85.4, 86.3, 84.7, 84.9, 85.8],
[34, 81.4, 82.1, 82.1, 83.5, 83.5, 83.3, 83.2, 83.5, 84.0, 84.8, 83.3, 83.3, 84.2],
[38, 80.2, 80.8, 80.9, 82.3, 82.3, 82.1, 81.9, 82.2, 82.6, 83.4, 81.8, 81.6, 82.5],
[42, 79.0, 79.6, 79.7, 81.1, 81.1, 80.9, 80.6, 80.8, 81.3, 81.9, 80.4, 80.0, 80.9],
[46, 77.8, 78.3, 78.5, 79.9, 79.8, 79.7, 79.3, 79.4, 79.9, 80.4, 78.9, 78.4, 79.2],
[50, 76.6, 77.0, 77.3, 78.7, 78.6, 78.5, 78.1, 78.0, 78.6, 78.9, 77.5, 76.8, 77.6],
[54, 75.4, 75.7, 76.2, 77.5, 77.3, 77.2, 76.8, 76.6, 77.2, 77.5, 76.1, 75.2, 75.9],
[58, 74.2, 74.5, 75.0, 76.3, 76.1, 76.0, 75.5, 75.3, 75.9, 76.0, 74.6, 73.6, 74.3],
],
/**
* Table 1502 - CN2 vs CN1 @ Mach 0, 0.2, 0.9
* n2_to_n1_table
* @param i row index (n2)
* @param j 1 = Mach 0, 2 = Mach 0.2, 3 = Mach 0.9
* @returns Corrected N1 (CN1)
*/
table1502: [
[0, 0, 0.2, 0.9],
[18.2, 0.0, 0.0, 17.0],
[22.0, 1.9, 1.9, 17.4],
[26.0, 2.5, 2.5, 18.2],
[57.0, 12.8, 12.8, 27.0],
[68.2, 19.6, 19.6, 34.827774],
[77.0, 26.0, 26.0, 40.839552],
[83.0, 31.42024, 31.42024, 44.768766],
[89.0, 40.972041, 40.972041, 50.09214],
[92.8, 51.0, 51.0, 55.042],
[97.0, 65.0, 65.0, 65.0],
[100.0, 77.0, 77.0, 77.0],
[104.0, 85.0, 85.0, 85.5],
[116.5, 101.0, 101.0, 101.0],
],
/**
* Table 1503 - Turbine LoMach (0) CN2 vs. Throttle @ IAP Ratio 1.00000000, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313
* mach_0_corrected_commanded_ne_table
* @param i row index (thrust lever position)
* @param j IAP ratio
* @returns Corrected N2 (CN2)
*/
table1503: [
[0, 1.0, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313],
[0.0, 68.2, 69.402657, 70.671269, 73.432244, 76.544349, 78.644882, 78.644882],
[0.1, 76.0, 77.340205, 78.753906, 81.830654, 85.298688, 87.639458, 87.639458],
[0.2, 83.0, 84.463645, 86.007556, 89.367688, 93.155146, 95.711513, 95.711513],
[0.4, 92.8, 94.436461, 96.162664, 99.919535, 104.154188, 107.01239, 107.01239],
[0.6, 98.0, 99.728159, 101.55109, 105.518475, 109.990414, 113.008774, 113.008774],
[0.75, 101.5, 103.289879, 105.177914, 109.286991, 113.918643, 117.044802, 117.044802],
[0.9, 103.0, 104.81633, 106.0, 110.90207, 115.60217, 118.774528, 118.774528],
[1.0, 104.2, 106.037491, 107.97575, 112.194133, 116.948991, 120.158309, 120.158309],
],
/**
* Table 1504 - Turbine HiMach (0.9) CN2 vs. Throttle @ IAP Ratio 1.00000000, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313
* mach_hi_corrected_commanded_ne_table
* @param i row index (thrust lever position)
* @param j IAP ratio
* @returns Corrected N2 (CN2)
*/
table1504: [
[0, 1.0, 1.20172257, 1.453783983, 2.175007333, 3.364755652, 4.47246108, 5.415178313],
[0.0, 63.267593, 64.383271, 65.560133, 68.121427, 71.008456, 72.957073, 72.957073],
[0.1, 70.503476, 71.746753, 73.058212, 75.912441, 79.129658, 81.301137, 81.301137],
[0.2, 76.997217, 78.355007, 79.787258, 82.904376, 86.417916, 88.789399, 88.789399],
[0.4, 86.088455, 87.606562, 89.207922, 92.693086, 96.621477, 99.272967, 99.272967],
[0.6, 90.912377, 92.51555, 94.206642, 97.887095, 102.035612, 104.835676, 104.835676],
[0.75, 94.159247, 95.819677, 97.571165, 101.383063, 105.679741, 108.579808, 108.579808],
[0.9, 95.550763, 97.235732, 98.333795, 102.881334, 107.24151, 110.184435, 110.184435],
[1.0, 104.2, 106.037491, 107.97575, 112.194133, 116.948991, 120.158309, 120.158309],
],
/**
* Table 1506 - Corrected net Thrust vs CN1 @ Mach 0 to 0.9 in 0.1 steps
* n1_and_mach_on_thrust_table
* @param i row index (CN1)
* @param j mach
* @returns Corrected net thrust (pounds of force)
*/
table1506: [
[0, 0, 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9],
[0, 0.015, -0.15, 0, 0, 0, 0, 0, 0, 0, 0],
[20, 0.1286, -0.008, 0.015, 0.0337152, -0.0207408, -0.0447408, -0.0684924, -0.2470092, -0.3784788, -0.5864604],
[25, 0.155, 0.0236, 0.018, 0.0364848, -0.0115116, -0.0318852, -0.0503988, -0.1815936, -0.3194448, -0.5268336],
[30.0, 0.16, 0.16, 0.02, 0.039, 0.01, -0.01, -0.02, -0.107, -0.195, -0.428],
[35.0, 0.315, 0.151, 0.093, 0.055, 0.03, 0.013, -0.002, -0.083, -0.164, -0.394],
[40.0, 0.396, 0.195, 0.149, 0.07, 0.043, 0.05, 0.03, -0.051, -0.121, -0.342],
[45.0, 0.472, 0.3, 0.188, 0.11, 0.07, 0.1, 0.06, -0.012, -0.069, -0.275],
[50.0, 0.543, 0.373, 0.254, 0.13, 0.125, 0.16, 0.11, 0.033, -0.01, -0.196],
[55.0, 0.611, 0.448, 0.324, 0.18, 0.155, 0.21, 0.21, 0.085, 0.055, -0.107],
[60.0, 0.714, 0.528, 0.402, 0.25, 0.165, 0.22, 0.26, 0.15, 0.124, -0.012],
[65.0, 0.792, 0.615, 0.489, 0.32, 0.21, 0.23, 0.28, 0.27, 0.196, 0.087],
[70.0, 0.88, 0.712, 0.586, 0.38, 0.28, 0.235, 0.31, 0.34, 0.267, 0.184],
[75.0, 0.982, 0.821, 0.695, 0.43, 0.39, 0.3, 0.32, 0.36, 0.39, 0.27],
[80.0, 1.092, 0.941, 0.811, 0.55, 0.45, 0.4, 0.4, 0.38, 0.44, 0.37],
[85.0, 1.23, 1.07, 0.932, 0.66, 0.57, 0.48, 0.55, 0.48, 0.49, 0.45],
[90.0, 1.388, 1.206, 1.049, 0.75, 0.68, 0.56, 0.64, 0.62, 0.57, 0.59],
[95.0, 1.538, 1.34, 1.153, 0.875, 0.75, 0.6, 0.68, 0.69, 0.66, 0.69],
[100.0, 1.603, 1.465, 1.229, 0.95, 0.8, 0.7, 0.74, 0.74, 0.68, 0.75],
[105.0, 1.655, 1.488, 1.258, 1.03, 0.859, 0.8, 0.82, 0.77, 0.69, 0.77],
[110.0, 1.671, 1.503, 1.283, 1.1, 0.935, 0.9, 0.92, 0.8, 0.71, 0.78],
],
};

const fmsSymbolConfig: FMSymbolsConfig = {
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