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FMGC: Rework VLS and other speeds significantly, AP and A/THR now respect VLS and VMAX

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This commit is contained in:
Josh Davidson 2022-01-09 20:22:57 -05:00
parent d68988def7
commit b71db001b3
10 changed files with 372 additions and 128 deletions
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1
A320-main.xml
View file

@ -841,6 +841,7 @@
<cost-index type="int">0</cost-index>
<flex type="int">45</flex>
<to-state type="bool">0</to-state>
<vmax type="double">350</vmax>
</internal>
<simbrief-username type="string"></simbrief-username>
</FMGC>

8
Models/Instruments/PFD/PFD.nas
View file

@ -85,6 +85,7 @@ var canvas_pfd = {
tgt_kts: 0,
tgt_ias: 0,
vapp: 0,
vls: 0,
new: func(svg, name, number) {
var obj = {parents: [canvas_pfd] };
obj.canvas = canvas.new({
@ -788,12 +789,13 @@ var canvas_pfd = {
}
if (!fmgc.FMGCInternal.takeoffState and fmgc.FMGCInternal.phase >= 1 and !notification.gear1Wow and !notification.gear2Wow) {
if (fmgc.FMGCInternal.vls_min <= 30) {
me.vls = fmgc.FMGCNodes.vls.getValue();
if (me.vls <= 30) {
me.VLSmin = 0 - me.ASI;
} else if (fmgc.FMGCInternal.vls_min >= 420) {
} else if (me.vls >= 420) {
me.VLSmin = 390 - me.ASI;
} else {
me.VLSmin = fmgc.FMGCInternal.vls_min - 30 - me.ASI;
me.VLSmin = me.vls - 30 - me.ASI;
}
if (fmgc.FMGCInternal.alpha_prot <= 30) {

4
Nasal/FMGC/FMGC-b.nas
View file

@ -262,10 +262,6 @@ var ITAF = {
Internal.vsTemp = Internal.vs.getValue();
Position.indicatedAltitudeFtTemp = Position.indicatedAltitudeFt.getValue();
# Update VLS / VMAX for autothrust
FMGCNodes.vmax.setValue(FMGCInternal.maxspeed);
FMGCNodes.vlsMin.setValue(FMGCInternal.vls_min);
# LNAV Engagement
if (Output.lnavArm.getBoolValue()) {
me.checkLnav(1);

130
Nasal/FMGC/FMGC.nas
View file

@ -55,6 +55,7 @@ var FMGCinit = func {
FMGCInternal.takeoffState = 0;
FMGCInternal.minspeed = 0;
FMGCInternal.maxspeed = 338;
FMGCNodes.vmax.setValue(338);
FMGCInternal.phase = 0; # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done
FMGCNodes.phase.setValue(0);
FMGCInternal.mngSpd = 157;
@ -257,17 +258,27 @@ var postInit = func() {
var FMGCNodes = {
costIndex: props.globals.initNode("/FMGC/internal/cost-index", 0, "DOUBLE"),
decel: props.globals.initNode("/FMGC/internal/decel", 0, "BOOL"),
flap2: props.globals.getNode("/FMGC/internal/flap-2"),
flap3: props.globals.getNode("/FMGC/internal/flap-3"),
mngSpdAlt: props.globals.getNode("/FMGC/internal/mng-alt-spd"),
ktsToMachFactor: props.globals.getNode("/FMGC/internal/kts-to-mach-factor"),
machToKtsFactor: props.globals.getNode("/FMGC/internal/mach-to-kts-factor"),
mngMachAlt: props.globals.getNode("/FMGC/internal/mng-alt-mach"),
slat: props.globals.getNode("/FMGC/internal/slat"),
toFromSet: props.globals.initNode("/FMGC/internal/tofrom-set", 0, "BOOL"),
toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
v1: props.globals.initNode("/FMGC/internal/v1", 0, "DOUBLE"),
v1set: props.globals.initNode("/FMGC/internal/v1-set", 0, "BOOL"),
phase: props.globals.initNode("/FMGC/internal/phase", 0, "INT"),
vlsMin: props.globals.initNode("/FMGC/internal/vls-min", 0, "DOUBLE"),
vmax: props.globals.initNode("/FMGC/internal/vmax", 0, "DOUBLE"),
vls: props.globals.getNode("/FMGC/internal/vls"),
vmax: props.globals.getNode("/FMGC/internal/vmax"),
vs1g: props.globals.getNode("/FMGC/internal/vs1g"),
vs1gConf0: props.globals.getNode("/FMGC/internal/vs1g-conf-0"),
vs1gConf1: props.globals.getNode("/FMGC/internal/vs1g-conf-1"),
vs1gConf1f: props.globals.getNode("/FMGC/internal/vs1g-conf-1f"),
vs1gConf2: props.globals.getNode("/FMGC/internal/vs1g-conf-2"),
vs1gConf3: props.globals.getNode("/FMGC/internal/vs1g-conf-3"),
vs1gConfFull: props.globals.getNode("/FMGC/internal/vs1g-conf-full"),
};
############
@ -558,7 +569,6 @@ var radios = maketimer(1, func() {
var newphase = nil;
var masterFMGC = maketimer(0.2, func {
n1_left = pts.Engines.Engine.n1Actual[0].getValue();
n1_right = pts.Engines.Engine.n1Actual[1].getValue();
modelat = Modes.PFD.FMA.rollMode.getValue();
@ -638,6 +648,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.maxspeed = fmgc.FMGCInternal.vmo_mmo.getValue();
}
FMGCNodes.vmax.setValue(FMGCInternal.maxspeed);
if (newphase != FMGCInternal.phase) { # phase changed
FMGCInternal.phase = newphase;
@ -693,6 +704,19 @@ var masterFMGC = maketimer(0.2, func {
}
}
# Speeds
FMGCInternal.vsw = FMGCNodes.vs1g.getValue();
FMGCInternal.vls = FMGCNodes.vls.getValue();
FMGCInternal.vs1g_conf_0 = FMGCNodes.vs1gConf0.getValue();
FMGCInternal.vs1g_conf_1 = FMGCNodes.vs1gConf1.getValue();
FMGCInternal.vs1g_conf_1f = FMGCNodes.vs1gConf1f.getValue();
FMGCInternal.vs1g_conf_2 = FMGCNodes.vs1gConf2.getValue();
FMGCInternal.vs1g_conf_3 = FMGCNodes.vs1gConf3.getValue();
FMGCInternal.vs1g_conf_full = FMGCNodes.vs1gConfFull.getValue();
FMGCInternal.slat = FMGCNodes.slat.getValue();
FMGCInternal.flap2 = FMGCNodes.flap2.getValue();
FMGCInternal.flap3 = FMGCNodes.flap3.getValue();
############################
# calculate speeds
############################
@ -700,27 +724,6 @@ var masterFMGC = maketimer(0.2, func {
weight_lbs = pts.Fdm.JSBsim.Inertia.weightLbs.getValue() / 1000;
altitude = pts.Instrumentation.Altimeter.indicatedFt.getValue();
# current speeds
FMGCInternal.clean = 2 * weight_lbs * 0.45359237 + 85;
if (altitude > 20000) {
FMGCInternal.clean += (altitude - 20000) / 1000;
}
FMGCInternal.vs1g_clean = 0.0024 * weight_lbs * weight_lbs + 0.124 * weight_lbs + 88.942;
FMGCInternal.vs1g_conf_1 = -0.0007 * weight_lbs * weight_lbs + 0.6795 * weight_lbs + 44.673;
FMGCInternal.vs1g_conf_1f = -0.0001 * weight_lbs * weight_lbs + 0.5211 * weight_lbs + 49.027;
FMGCInternal.vs1g_conf_2 = -0.0005 * weight_lbs * weight_lbs + 0.5488 * weight_lbs + 44.279;
FMGCInternal.vs1g_conf_3 = -0.0005 * weight_lbs * weight_lbs + 0.5488 * weight_lbs + 43.279;
FMGCInternal.vs1g_conf_full = -0.0007 * weight_lbs * weight_lbs + 0.6002 * weight_lbs + 38.479;
FMGCInternal.slat = FMGCInternal.vs1g_clean * 1.23;
FMGCInternal.flap2 = FMGCInternal.vs1g_conf_2 * 1.47;
FMGCInternal.flap3 = FMGCInternal.vs1g_conf_3 * 1.36;
if (FMGCInternal.ldgConfig3) {
FMGCInternal.vls = math.clamp(FMGCInternal.vs1g_conf_3 * 1.23, 113, 999);
} else {
FMGCInternal.vls = math.clamp(FMGCInternal.vs1g_conf_full * 1.23, 113, 999);
}
if (!fmgc.FMGCInternal.vappSpeedSet) {
if (FMGCInternal.destWind < 5) {
FMGCInternal.vapp = FMGCInternal.vls + 5;
@ -734,7 +737,7 @@ var masterFMGC = maketimer(0.2, func {
# predicted takeoff speeds
if (FMGCInternal.phase == 1) {
FMGCInternal.clean_to = FMGCInternal.clean;
FMGCInternal.vs1g_clean_to = FMGCInternal.vs1g_clean;
FMGCInternal.vs1g_conf_0_to = FMGCInternal.vs1g_conf_0;
FMGCInternal.vs1g_conf_2_to = FMGCInternal.vs1g_conf_2;
FMGCInternal.vs1g_conf_3_to = FMGCInternal.vs1g_conf_3;
FMGCInternal.vs1g_conf_full_to = FMGCInternal.vs1g_conf_full;
@ -745,18 +748,18 @@ var masterFMGC = maketimer(0.2, func {
if (altitude > 20000) {
FMGCInternal.clean_to += (altitude - 20000) / 1000;
}
FMGCInternal.vs1g_clean_to = 0.0024 * FMGCInternal.tow * FMGCInternal.tow + 0.124 * FMGCInternal.tow + 88.942;
FMGCInternal.vs1g_conf_0_to = 0.0024 * FMGCInternal.tow * FMGCInternal.tow + 0.124 * FMGCInternal.tow + 88.942;
FMGCInternal.vs1g_conf_2_to = -0.0005 * FMGCInternal.tow * FMGCInternal.tow + 0.5488 * FMGCInternal.tow + 44.279;
FMGCInternal.vs1g_conf_3_to = -0.0005 * FMGCInternal.tow * FMGCInternal.tow + 0.5488 * FMGCInternal.tow + 43.279;
FMGCInternal.vs1g_conf_full_to = -0.0007 * FMGCInternal.tow * FMGCInternal.tow + 0.6002 * FMGCInternal.tow + 38.479;
FMGCInternal.slat_to = FMGCInternal.vs1g_clean_to * 1.23;
FMGCInternal.slat_to = FMGCInternal.vs1g_conf_0_to * 1.23;
FMGCInternal.flap2_to = FMGCInternal.vs1g_conf_2_to * 1.47;
}
# predicted approach (temp go-around) speeds
if (FMGCInternal.phase == 5 or FMGCInternal.phase == 6) {
FMGCInternal.clean_appr = FMGCInternal.clean;
FMGCInternal.vs1g_clean_appr = FMGCInternal.vs1g_clean;
FMGCInternal.vs1g_conf_0_appr = FMGCInternal.vs1g_conf_0;
FMGCInternal.vs1g_conf_2_appr = FMGCInternal.vs1g_conf_2;
FMGCInternal.vs1g_conf_3_appr = FMGCInternal.vs1g_conf_3;
FMGCInternal.vs1g_conf_full_appr = FMGCInternal.vs1g_conf_full;
@ -771,11 +774,11 @@ var masterFMGC = maketimer(0.2, func {
if (altitude > 20000) {
FMGCInternal.clean_appr += (altitude - 20000) / 1000;
}
FMGCInternal.vs1g_clean_appr = 0.0024 * FMGCInternal.lw * FMGCInternal.lw + 0.124 * FMGCInternal.lw + 88.942;
FMGCInternal.vs1g_conf_0_appr = 0.0024 * FMGCInternal.lw * FMGCInternal.lw + 0.124 * FMGCInternal.lw + 88.942;
FMGCInternal.vs1g_conf_2_appr = -0.0005 * FMGCInternal.lw * FMGCInternal.lw + 0.5488 * FMGCInternal.lw + 44.279;
FMGCInternal.vs1g_conf_3_appr = -0.0005 * FMGCInternal.lw * FMGCInternal.lw + 0.5488 * FMGCInternal.lw + 43.279;
FMGCInternal.vs1g_conf_full_appr = -0.0007 * FMGCInternal.lw * FMGCInternal.lw + 0.6002 * FMGCInternal.lw + 38.479;
FMGCInternal.slat_appr = FMGCInternal.vs1g_clean_appr * 1.23;
FMGCInternal.slat_appr = FMGCInternal.vs1g_conf_0_appr * 1.23;
FMGCInternal.flap2_appr = FMGCInternal.vs1g_conf_2_appr * 1.47;
if (FMGCInternal.ldgConfig3) {
FMGCInternal.vls_appr = FMGCInternal.vs1g_conf_3_appr * 1.23;
@ -796,8 +799,6 @@ var masterFMGC = maketimer(0.2, func {
}
}
# Need info on these, also correct for height at altitude...
# https://www.pprune.org/archive/index.php/t-587639.html
aoa_prot = 15;
aoa_max = 17.5;
aoa_0 = -5;
@ -811,70 +812,6 @@ var masterFMGC = maketimer(0.2, func {
FMGCInternal.alpha_max = 0;
}
#FMGCInternal.vs1g_conf_2_appr = FMGCInternal.vs1g_conf_2;
#FMGCInternal.vs1g_conf_3_appr = FMGCInternal.vs1g_conf_3;
#FMGCInternal.vs1g_conf_full_appr = FMGCInternal.vs1g_conf_full;
if (flap == 0) { # 0
FMGCInternal.vsw = FMGCInternal.vs1g_clean;
FMGCInternal.minspeed = FMGCInternal.clean;
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.28;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.23;
}
} elsif (flap == 1) { # 1
FMGCInternal.vsw = FMGCInternal.vs1g_conf_2;
FMGCInternal.minspeed = FMGCInternal.slat;
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_1 * 1.28;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_1 * 1.23;
}
} elsif (flap == 2) { # 1+F
FMGCInternal.vsw = FMGCInternal.vs1g_conf_1f;
FMGCInternal.minspeed = FMGCInternal.slat;
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.13;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_1f * 1.23;
}
} elsif (flap == 3) { # 2
FMGCInternal.vsw = FMGCInternal.vs1g_conf_2;
FMGCInternal.minspeed = FMGCInternal.flap2;
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.13;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_2 * 1.23;
}
} elsif (flap == 4) { # 3
FMGCInternal.vsw = FMGCInternal.vs1g_conf_3;
FMGCInternal.minspeed = FMGCInternal.flap3;
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.13;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_3 * 1.23;
}
} elsif (flap == 5) { # FULL
FMGCInternal.vsw = FMGCInternal.vs1g_conf_full;
if (FMGCInternal.vappSpeedSet) {
FMGCInternal.minspeed = FMGCInternal.vapp_appr;
} else {
FMGCInternal.minspeed = FMGCInternal.vapp;
}
if (FMGCInternal.takeoffState) {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.13;
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_full * 1.23;
}
}
if (gear0 and flap < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
if (!FMGCInternal.takeoffState) {
fmgc.FMGCNodes.toState.setValue(1);
@ -886,7 +823,6 @@ var masterFMGC = maketimer(0.2, func {
}
FMGCInternal.takeoffState = 0;
}
});
############################

2
Systems/a320-adr.xml
View file

@ -759,7 +759,7 @@
<property>/systems/navigation/adr/output/cas-3</property>
</max>
<difference>
<property>/FMGC/internal/vls-min</property>
<property>/FMGC/internal/vls</property>
<property>/systems/navigation/adr/computation/underspeed-difference</property>
</difference>
</lt>

290
Systems/a320-fmgc.xml
View file

@ -7,8 +7,9 @@
<property value="350">/FMGC/internal/vmo-kts</property>
<channel name="FMGC" execrate="8">
<channel name="Envelope Protection" execrate="8">
<!-- Vmo/Mmo -->
<fcs_function name="/FMGC/internal/mmo-kts">
<function>
<product>
@ -16,7 +17,7 @@
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
<max> <!-- Prevent divide by 0 -->
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
<value>0.0000001</value>
<value>0.0001</value>
</max>
</quotient>
<value>0.82</value>
@ -41,6 +42,290 @@
</function>
</fcs_function>
<!-- VS1g -->
<fcs_function name="/FMGC/internal/vs1g-kts">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<independentVar lookup="table">fcs/slat-pos-deg</independentVar>
<tableData breakPoint="0"> <!-- 40 column is a guess, no data for flap without slat -->
0 40
35000 114.99 99.55
40000 123.08 106.14
45000 130.66 111.83
50000 137.73 117.76
55000 144.41 123.46
60000 150.81 128.89
65000 156.76 133.34
70000 162.65 138.73
75000 168.43 143.60
80000 173.65 148.02
</tableData>
<tableData breakPoint="27">
0 10 15 20 35 40
35000 95.11 90.08 85.16 83.55 81.61 79.67
40000 101.59 96.03 90.31 88.77 86.71 84.65
45000 107.89 101.93 95.64 94.32 91.69 89.06
50000 113.84 107.55 101.02 99.25 96.56 93.87
55000 119.46 112.76 106.07 104.23 101.37 98.51
60000 124.84 117.97 110.94 109.10 106.01 102.92
65000 130.17 122.96 115.63 113.75 110.25 106.75
70000 135.10 127.54 119.99 118.16 114.67 111.18
75000 139.91 132.18 124.23 122.28 118.68 115.08
80000 144.44 136.54 128.58 126.35 122.58 118.81
</tableData>
</table>
</function>
</fcs_function>
<!-- Extra VS1g tables for predictions etc -->
<fcs_function name="/FMGC/internal/vs1g-conf-0">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<tableData>
35000 114.99
40000 123.08
45000 130.66
50000 137.73
55000 144.41
60000 150.81
65000 156.76
70000 162.65
75000 168.43
80000 173.65
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-conf-1">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<tableData>
35000 95.11
40000 101.59
45000 107.89
50000 113.84
55000 119.46
60000 124.84
65000 130.17
70000 135.10
75000 139.91
80000 144.44
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-conf-1f">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<tableData>
35000 90.08
40000 96.03
45000 101.93
50000 107.55
55000 112.76
60000 117.97
65000 122.96
70000 127.54
75000 132.18
80000 136.54
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-conf-2">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<tableData>
35000 85.16
40000 90.31
45000 95.64
50000 101.02
55000 106.07
60000 110.94
65000 115.63
70000 119.99
75000 124.23
80000 128.58
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-conf-3">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<tableData>
35000 83.55
40000 88.77
45000 94.32
50000 99.25
55000 104.23
60000 109.10
65000 113.75
70000 118.16
75000 122.28
80000 126.35
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-conf-full">
<function>
<table>
<independentVar lookup="row">inertia/weight-kg</independentVar>
<independentVar lookup="column">/options/maxflap</independentVar>
<tableData> <!-- CFM 35, IAE 40 -->
35 40
35000 81.61 79.67
40000 86.71 84.65
45000 91.69 89.06
50000 96.56 93.87
55000 101.37 98.51
60000 106.01 102.92
65000 110.25 106.75
70000 114.67 111.18
75000 118.68 115.08
80000 122.58 118.81
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="/FMGC/internal/vs1g-roll-factor">
<function>
<sqrt> <!-- Take the square root to get the factor -->
<quotient> <!-- Calculate neutral load factor from bank -->
<value>1</value>
<cos>
<toradians>
<min>
<abs>
<property>/orientation/roll-deg</property>
</abs>
<value>89</value> <!-- Above math breaks -->
</min>
</toradians>
</cos>
</quotient>
</sqrt>
</function>
</fcs_function>
<pure_gain name="/FMGC/internal/vs1g">
<input>/FMGC/internal/vs1g-kts</input>
<gain>/FMGC/internal/vs1g-roll-factor</gain>
<clipto>
<min>0</min>
<max>/FMGC/internal/vmo-mmo</max>
</clipto>
</pure_gain>
<!-- Vls -->
<switch name="/FMGC/internal/takeoff-latch">
<default value="/FMGC/internal/takeoff-latch"/>
<test logic="OR" value="1">
position/wow eq 1
/FMGC/internal/phase lt 2
/FMGC/internal/phase eq 6
</test>
<test value="0">
fcs/flap-pos-deg lt 0.1
</test>
</switch>
<switch name="/FMGC/internal/vls-factor">
<default value="1.23"/> <!-- 1.23 VS1g -->
<test value="1.13"> <!-- 1.13 VS1g -->
/FMGC/internal/takeoff-latch eq 1
</test>
</switch>
<fcs_function name="/FMGC/internal/vls">
<function>
<product>
<property>/FMGC/internal/vs1g-kts</property>
<sum>
<property>/FMGC/internal/vls-factor</property>
<table>
<independentVar lookup="row">atmosphere/density-altitude</independentVar>
<tableData>
0 0.00
43000 0.22
</tableData>
</table>
</sum>
</product>
</function>
<clipto>
<min>/FMGC/internal/vs1g</min>
<max>100000</max>
</clipto>
</fcs_function>
<fcs_function name="/FMGC/internal/vls-mach">
<function>
<product>
<quotient>
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
<max> <!-- Prevent divide by 0 -->
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
<value>0.0001</value>
</max>
</quotient>
<property>/FMGC/internal/vls</property>
</product>
</function>
</fcs_function>
<!-- Vmax - Computed in FMGC.nas and ADR.nas -->
<fcs_function name="/FMGC/internal/vmax-mach">
<function>
<product>
<quotient>
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
<max> <!-- Prevent divide by 0 -->
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
<value>0.0001</value>
</max>
</quotient>
<property>/FMGC/internal/vmax</property>
</product>
</function>
</fcs_function>
<!-- Slat -->
<pure_gain name="/FMGC/internal/slat">
<input>/FMGC/internal/vs1g-conf-1</input>
<gain>1.22</gain>
</pure_gain>
<!-- Flap 2 -->
<pure_gain name="/FMGC/internal/flap-2">
<input>/FMGC/internal/vs1g-conf-2</input>
<gain>1.25</gain>
</pure_gain>
<!-- Flap 3 -->
<pure_gain name="/FMGC/internal/flap-3">
<input>/FMGC/internal/vs1g-conf-3</input>
<gain>1.25</gain>
</pure_gain>
</channel>
<channel name="FMGC Misc" execrate="8">
<fcs_function name="/systems/fmgc/cas-compare/cas-1-to-3">
<function>
<abs>
@ -259,6 +544,7 @@
</ifthen>
</function>
</fcs_function>
</channel>
</system>

11
Systems/a320-libraries.xml
View file

@ -28,7 +28,7 @@
</test>
</switch>
<fcs_function name="/position/gear-agl-ft-tie">
<fcs_function name="position/gear-agl-ft">
<function>
<difference>
<property>/position/altitude-agl-ft</property>
@ -38,11 +38,16 @@
<output>/position/gear-agl-ft</output> <!-- So flight recorder can override it -->
</fcs_function>
<pure_gain name="/position/gear-agl-m-tie">
<input>/position/gear-agl-ft</input>
<pure_gain name="position/gear-agl-m">
<input>position/gear-agl-ft</input>
<gain>0.3048</gain>
<output>/position/gear-agl-m</output> <!-- So flight recorder can override it -->
</pure_gain>
<pure_gain name="inertia/weight-kg">
<input>inertia/weight-lbs</input>
<gain>0.45359237</gain>
</pure_gain>
</channel>

16
Systems/fmgc-drivers.xml
View file

@ -239,7 +239,13 @@
<expression>
<product>
<difference>
<property>/it-autoflight/input/mach</property>
<max>
<min>
<property>/it-autoflight/input/mach</property>
<property>/FMGC/internal/vmax-mach</property>
</min>
<property>/FMGC/internal/vls-mach</property>
</max>
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
</difference>
<value>80</value>
@ -250,7 +256,13 @@
<expression>
<product>
<difference>
<property>/it-autoflight/input/kts</property>
<max>
<min>
<property>/it-autoflight/input/kts</property>
<property>/FMGC/internal/vmax</property>
</min>
<property>/FMGC/internal/vls</property>
</max>
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
</difference>
<value>0.08</value>

24
Systems/fmgc-thrust.xml
View file

@ -10,7 +10,17 @@
<debug>false</debug>
<type>gain</type>
<gain>1.0</gain>
<input>/it-autoflight/input/kts</input>
<input>
<expression>
<max>
<min>
<property>/it-autoflight/input/kts</property>
<property>/FMGC/internal/vmax</property>
</min>
<property>/FMGC/internal/vls</property>
</max>
</expression>
</input>
<output>/it-autoflight/internal/athr-kts-cmd</output>
<min>
<expression>
@ -72,7 +82,17 @@
<debug>false</debug>
<type>gain</type>
<gain>1.0</gain>
<input>/it-autoflight/input/mach</input>
<input>
<expression>
<max>
<min>
<property>/it-autoflight/input/mach</property>
<property>/FMGC/internal/vmax-mach</property>
</min>
<property>/FMGC/internal/vls-mach</property>
</max>
</expression>
</input>
<output>/it-autoflight/internal/athr-mach-cmd</output>
<min>
<expression>

14
Systems/libraries.xml
View file

@ -577,20 +577,6 @@
<output>/systems/pressurization/targetvs</output>
</filter>
<filter>
<name>LBtoKG</name>
<type>gain</type>
<gain>1.0</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input>
<product>
<property>/fdm/jsbsim/inertia/weight-lbs</property>
<value>0.45359237</value>
</product>
</input>
<output>/fdm/jsbsim/inertia/weight-kg</output>
</filter>
<filter>
<name>optalt</name>
<type>gain</type>