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temp fdm shit

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This commit is contained in:
Josh Davidson 2020-11-23 12:54:32 -05:00
parent 69a7302f04
commit 49140e440c
12 changed files with 348 additions and 246 deletions
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2
A320-main.xml
View file

@ -489,7 +489,7 @@
<float n="6" alias="/fdm/jsbsim/hydraulics/aileron-l/final-deg"/>
<float n="7" alias="/fdm/jsbsim/hydraulics/aileron-r/final-deg"/>
<float n="8" alias="/fdm/jsbsim/hydraulics/rudder/final-deg"/>
<float n="9" alias="/fdm/jsbsim/hydraulics/elevator-trim/final-deg"/>
<float n="9" alias="/fdm/jsbsim/hydraulics/stabilizer/final-deg"/>
<float n="11" alias="/fdm/jsbsim/fcs/slat-pos-norm"/>
<float n="12" alias="/fdm/jsbsim/fcs/flap-pos-norm"/>
<int n="2" alias="/controls/lighting/landing-lights[0]"/>

2
AircraftConfig/fbw.xml
View file

@ -213,7 +213,7 @@
<slider>
<pref-height>150</pref-height>
<vertical>true</vertical>
<property>/fdm/jsbsim/hydraulics/elevator-trim/final-deg</property>
<property>/fdm/jsbsim/hydraulics/stabilizer/final-deg</property>
<min>-12.5</min>
<max>4</max>
<step>0.00125</step>

2
Models/FlightDeck/a320.flightdeck.xml
View file

@ -6177,7 +6177,7 @@
<animation>
<type>rotate</type>
<object-name>trim_2_lts</object-name>
<property>fdm/jsbsim/hydraulics/elevator-trim/cmd-deg</property>
<property>fdm/jsbsim/hydraulics/stabilizer/cmd-deg</property>
<factor>15.55</factor>
<offset-deg>1.4</offset-deg>
<axis>

4
Nasal/ECAM/ECAM-logic.nas
View file

@ -723,7 +723,7 @@ var messages_priority_3 = func {
ECAM_controller.warningReset(spd_brk_config_1);
}
if ((pitch_trim_config.clearFlag == 0) and (getprop("/fdm/jsbsim/hydraulics/elevator-trim/final-deg") > 1.75 or getprop("/fdm/jsbsim/hydraulics/elevator-trim/final-deg") < -3.65) and phaseVar3 >= 3 and phaseVar3 <= 4) {
if ((pitch_trim_config.clearFlag == 0) and (getprop("/fdm/jsbsim/hydraulics/stabilizer/final-deg") > 1.75 or getprop("/fdm/jsbsim/hydraulics/stabilizer/final-deg") < -3.65) and phaseVar3 >= 3 and phaseVar3 <= 4) {
pitch_trim_config.active = 1;
pitch_trim_config_1.active = 1;
} else {
@ -2028,7 +2028,7 @@ var messages_priority_0 = func {
var messages_config_memo = func {
phaseVarMemo = phaseNode.getValue();
if (getprop("/controls/flight/flaps-input") == 0 or getprop("/controls/flight/flaps-input") == 4 or pts.Controls.Flight.speedbrake.getValue() != 0 or getprop("/fdm/jsbsim/hydraulics/elevator-trim/final-deg") > 1.75 or getprop("/fdm/jsbsim/hydraulics/elevator-trim/final-deg") < -3.65 or getprop("/fdm/jsbsim/hydraulics/rudder/trim-cmd-deg") < -3.55 or getprop("/fdm/jsbsim/hydraulics/rudder/trim-cmd-deg") > 3.55) {
if (getprop("/controls/flight/flaps-input") == 0 or getprop("/controls/flight/flaps-input") == 4 or pts.Controls.Flight.speedbrake.getValue() != 0 or getprop("/fdm/jsbsim/hydraulics/stabilizer/final-deg") > 1.75 or getprop("/fdm/jsbsim/hydraulics/stabilizer/final-deg") < -3.65 or getprop("/fdm/jsbsim/hydraulics/rudder/trim-cmd-deg") < -3.55 or getprop("/fdm/jsbsim/hydraulics/rudder/trim-cmd-deg") > 3.55) {
setprop("/ECAM/to-config-normal", 0);
} else {
setprop("/ECAM/to-config-normal", 1);

2
Nasal/FBW/it-fbw.nas
View file

@ -188,7 +188,7 @@ var update_loop = func {
}
if (systems.ELEC.EmerElec.getBoolValue()) {
if (lawyaw == 0 or lawyaw == 1) {
} elsif (fac1 and lawyaw == 2) {
} else if (fac1 and lawyaw == 2) {
FBW.degradeYawLaw.setValue(1);
}
if (law == 0) {

2
Nasal/Libraries/libraries.nas
View file

@ -462,7 +462,7 @@ setlistener("/controls/flight/elevator-trim", func {
# For the cockpit rotation and anywhere else you want to use it
var cmdDegCalc = 0;
var slewPitchWheel = func(d) {
cmdDegCalc = math.round(pts.Fdm.JSBsim.Hydraulics.ElevatorTrim.cmdDeg.getValue(), 0.1);
cmdDegCalc = math.round(pts.Fdm.JSBsim.Hydraulics.Stabilizer.cmdDeg.getValue(), 0.1);
if (d > 0) { # DN
if (cmdDegCalc < 4) {
cmdDegCalc = (cmdDegCalc + 0.1) / 13.5; # Add and normalize, NOT 4! 13.5 = 1 on either polarity

6
Nasal/Libraries/property-tree-setup.nas
View file

@ -97,12 +97,12 @@ var Fdm = {
elevator: props.globals.getNode("/fdm/jsbsim/fbw/elevator-sidestick"),
},
Hydraulics: {
ElevatorTrim: {
cmdDeg: props.globals.getNode("/fdm/jsbsim/hydraulics/elevator-trim/cmd-deg"),
},
Rudder: {
trimDeg: props.globals.getNode("/fdm/jsbsim/hydraulics/rudder/trim-deg"),
},
Stabilizer: {
cmdDeg: props.globals.getNode("/fdm/jsbsim/hydraulics/stabilizer/cmd-deg"),
},
},
Inertia: {
weightLbs: props.globals.getNode("/fdm/jsbsim/inertia/weight-lbs"),

556
Systems/a320-aerodynamics.xml
View file

@ -3,63 +3,148 @@
<!-- Airbus A320 Aerodynamics -->
<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
<aerodynamics>
<aerodynamics> <!-- WIP REWORK 2020 by Josh Davidson (Octal450) -->
<property value="0.0">ice/wingL</property>
<property value="0.0">ice/wingR</property>
<property value="0">ice/wingL</property>
<property value="0">ice/wingR</property>
<function name="aero/function/kCLge">
<description>Lift factor due to ground effect</description>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.00 1.203
0.10 1.127
0.15 1.090
0.20 1.073
0.30 1.046
0.40 1.055
0.50 1.019
0.60 1.013
0.70 1.008
0.80 1.006
0.90 1.003
1.00 1.002
1.10 1.000
</tableData>
</table>
</function>
<function name="aero/function/kCDge">
<description>Drag factor due to ground effect</description>
<table>
<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
<tableData>
0.00 0.480
0.10 0.515
0.15 0.629
0.20 0.709
0.30 0.815
0.40 0.882
0.50 0.928
0.60 0.962
0.70 0.988
0.80 1.000
</tableData>
</table>
</function>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<function name="aero/coefficient/CLalpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-1.57 -1.4000
-1.22 -1.3512
-1.05 -1.2426
-0.88 -1.1575
-0.64 -1.0312
-0.25 -0.9379
0.00 0.1494
0.25 1.6272
0.60 1.0305
0.88 0.6415
1.05 0.2294
1.22 0.0544
1.57 0.0000
-9.8475 -0.5652
-2.0912 0.0625
-0.0098 0.2386
2.2280 0.4260
4.2779 0.5779
6.4218 0.7540
8.4561 0.9163
9.2699 0.9842
10.7094 1.0843
11.6170 1.1538
12.6496 1.2184
13.7292 1.2911
14.7930 1.3444
15.6981 1.1882
16.6352 1.1064
17.5725 1.0311
18.6045 1.0447
19.6052 1.0479
30.1264 0.6376
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_pitch_rate">
<function name="aero/coefficient/CLq">
<description>Lift due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>velocities/q-aero-rad_sec</property>
<property>aero/ci2vel</property>
<value>6.9404</value>
<value>1.36</value>
</product>
</function>
<function name="aero/force/Lift_alpha_rate">
<function name="aero/coefficient/CLadot">
<description>Lift due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alphadot-rad_sec</property>
<property>aero/ci2vel</property>
<value>1.9706</value>
<value>0.6384</value>
</product>
</function>
<function name="aero/force/Lift_left_elevator">
<description>Lift due to left elevator deflection</description>
<function name="aero/coefficient/CLflap">
<description>Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">fcs/flap-pos-deg</independentVar>
<tableData>
0 0.0000
10 0.0948
15 0.1617
20 0.2704
40 0.3466
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLslat">
<description>Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">fcs/slat-pos-deg</independentVar>
<tableData>
0 0.0000
18 0.2334
22 0.2809
27 0.3323
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLde_l">
<description>Lift due to left elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -68,8 +153,8 @@
</product>
</function>
<function name="aero/force/Lift_right_elevator">
<description>Lift due to right elevator deflection</description>
<function name="aero/coefficient/CLde_r">
<description>Lift due to right elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -78,53 +163,18 @@
</product>
</function>
<function name="aero/force/Lift_elevator_trim_control">
<description>Lift due to elevator trim control deflection</description>
<function name="aero/coefficient/CLdstab">
<description>Lift due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/elevator-trim/final-deg</property></toradians>
<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>0.0118082</value>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.0000
0.290 0.0948
0.596 0.1617
0.645 0.2704
1.000 0.3466
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slat">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/slat-pos-norm</independentVar>
<tableData>
0.000 0.0000
0.666 0.2334
0.814 0.2809
1.000 0.3323
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_left_spoiler">
<description>Delta Lift due to left spoiler</description>
<function name="aero/coefficient/CLdsp_l">
<description>Lift due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -133,8 +183,8 @@
</product>
</function>
<function name="aero/force/Lift_right_spoiler">
<description>Delta Lift due to right spoiler</description>
<function name="aero/coefficient/CLdsp_r">
<description>Lift due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -143,8 +193,8 @@
</product>
</function>
<function name="aero/coefficient/CLicewl">
<description>Lift_decrease_due_to_ice_on_wing</description>
<function name="aero/coefficient/CLice_l">
<description>Lift due to left wing ice</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -160,15 +210,15 @@
</product>
</function>
<function name="aero/coefficient/CLicewr">
<description>Lift_decrease_due_to_ice_on_wing</description>
<function name="aero/coefficient/CLice_r">
<description>Lift due to right wing ice</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>ice/wingR</independentVar>
<tableData>
0.0 0.0
0.0 0.00
0.5 -0.05
1.0 -0.15
2.0 -1.25
@ -181,7 +231,7 @@
<axis name="DRAG">
<function name="aero/force/Drag_minimum">
<function name="aero/coefficient/CD0">
<description>Minimum drag</description>
<product>
<property>aero/qbar-psf</property>
@ -190,35 +240,42 @@
</product>
</function>
<function name="aero/force/Drag_alpha">
<function name="aero/coefficient/CDalpha">
<description>Drag due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-1.57 1.3083
-0.20 0.0301
0.00 0.0000
0.20 0.0301
1.57 1.3083
-14.7960 0.0549
-12.2922 0.0512
-9.4900 0.0379
-6.9768 0.0224
-3.2108 0.0049
0.0000 0.0000
3.2108 0.0049
6.9768 0.0224
9.4900 0.0379
12.2922 0.0512
14.7960 0.0549
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<function name="aero/coefficient/CDi">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<property>aero/cl-squared</property>
<value>0.0384</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<function name="aero/coefficient/CDmach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
@ -229,14 +286,14 @@
0.00 0.000
0.20 0.000
0.82 0.002
1.10 0.023
1.80 0.015
1.10 0.016
1.80 0.012
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_beta">
<function name="aero/coefficient/CDbeta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
@ -254,108 +311,38 @@
</product>
</function>
<function name="aero/force/Drag_left_elevator">
<description>Drag due to left elevator deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-l/final-deg</property></toradians></abs>
<value>0.00782</value>
</product>
</function>
<function name="aero/force/Drag_right_elevator">
<description>Drag due to right elevator deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-r/final-deg</property></toradians></abs>
<value>0.00782</value>
</product>
</function>
<function name="aero/force/Drag_elevator_trim_control">
<description>Drag due to elevator trim control deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-trim/final-deg</property></toradians></abs>
<value>0.01564</value>
</product>
</function>
<function name="aero/force/Drag_gear">
<function name="aero/coefficient/CDgear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.0175</value>
<value>0.0171</value>
</product>
</function>
<function name="aero/force/Drag_flap">
<function name="aero/coefficient/CDflap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value>0.00125</value>
<value>0.00122</value>
</product>
</function>
<function name="aero/force/Drag_slat">
<function name="aero/coefficient/CDslat">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value>0.00125</value>
<value>0.00118</value>
</product>
</function>
<function name="aero/force/Drag_left_aileron">
<description>Drag due to left aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-l/final-deg</property></toradians></abs>
<value>0.00811826141696</value>
</product>
</function>
<function name="aero/force/Drag_left_spoiler">
<description>Drag due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>0.025369566928</value>
</product>
</function>
<function name="aero/force/Drag_right_spoiler">
<description>Drag due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>0.025369566928</value>
</product>
</function>
<function name="aero/force/Drag_right_aileron">
<description>Drag due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-r/final-deg</property></toradians></abs>
<value>0.00811826141696</value>
</product>
</function>
<function name="aero/force/Drag_wingicel">
<description>Drag_due_to_ice_on_wing</description>
<function name="aero/coefficient/CDice_l">
<description>Drag due to left wing ice</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -371,8 +358,8 @@
</product>
</function>
<function name="aero/force/Drag_wingicer">
<description>Drag_due_to_ice_on_wing</description>
<function name="aero/coefficient/CDice_r">
<description>Drag due to right wing ice</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
@ -388,7 +375,77 @@
</product>
</function>
<function name="aero/force/Drag_landing_light_left">
<function name="aero/coefficient/CDde_l">
<description>Drag due to left elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-l/final-deg</property></toradians></abs>
<value>0.002625</value>
</product>
</function>
<function name="aero/coefficient/CDde_r">
<description>Drag due to right elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/elevator-r/final-deg</property></toradians></abs>
<value>0.002625</value>
</product>
</function>
<function name="aero/coefficient/CDdstab">
<description>Drag due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/stabilizer/final-deg</property></toradians></abs>
<value>0.0039</value>
</product>
</function>
<function name="aero/coefficient/CDda_l">
<description>Drag due to left aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-l/final-deg</property></toradians></abs>
<value>0.0029271086286386</value>
</product>
</function>
<function name="aero/coefficient/CDda_r">
<description>Drag due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><toradians><property>hydraulics/aileron-r/final-deg</property></toradians></abs>
<value>0.0029271086286386</value>
</product>
</function>
<function name="aero/coefficient/CDdsp_l">
<description>Drag due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-left-deg</property></toradians>
<value>0.025369566928</value>
</product>
</function>
<function name="aero/coefficient/CDdsp_r">
<description>Drag due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>fcs/spoiler-right-deg</property></toradians>
<value>0.025369566928</value>
</product>
</function>
<function name="aero/coefficient/CDlt_l">
<description>Drag due to left landing light</description>
<product>
<property>aero/qbar-psf</property>
@ -398,7 +455,7 @@
</product>
</function>
<function name="aero/force/Drag_landing_light_right">
<function name="aero/coefficient/CDlt_r">
<description>Drag due to right landing light</description>
<product>
<property>aero/qbar-psf</property>
@ -412,7 +469,7 @@
<axis name="SIDE">
<function name="aero/force/Side_beta">
<function name="aero/coefficient/CYbeta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
@ -422,7 +479,7 @@
</product>
</function>
<function name="aero/force/Side_roll_rate">
<function name="aero/coefficient/CYp">
<description>Side force due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
@ -432,16 +489,16 @@
<table>
<independentVar lookup="row">aero/Re</independentVar>
<tableData>
25661346 0.2466
28227480 0.0178
38492020 0.0079
51187312 0.0045
29913298 0.3518
32904628 0.0352
44869948 0.0201
59461352 0.0094
</tableData>
</table>
</product>
</function>
<function name="aero/force/Side_yaw_rate">
<function name="aero/coefficient/CYr">
<description>Side force due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
@ -452,13 +509,13 @@
</product>
</function>
<function name="aero/force/Side_rudder">
<function name="aero/coefficient/CYdr">
<description>Side force due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
<value>-0.2653</value>
<value>-0.214</value>
</product>
</function>
@ -466,18 +523,29 @@
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<function name="aero/coefficient/Clbeta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
<property>aero/beta-deg</property>
<value>0.44</value>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.4412 -0.0034
-2.2116 -0.0038
0.1900 -0.0040
2.4828 -0.0043
4.9473 -0.0043
6.1394 -0.0044
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Roll_damp">
<function name="aero/coefficient/Clp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
@ -485,11 +553,11 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.47</value>
<value>-0.58</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<function name="aero/coefficient/Clr">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
@ -501,7 +569,7 @@
</product>
</function>
<function name="aero/moment/Roll_left_aileron">
<function name="aero/coefficient/Clda_l">
<description>Roll moment due to left aileron</description>
<product>
<property>aero/qbar-psf</property>
@ -512,7 +580,7 @@
</product>
</function>
<function name="aero/moment/Roll_right_aileron">
<function name="aero/coefficient/Clda_r">
<description>Roll moment due to right aileron</description>
<product>
<property>aero/qbar-psf</property>
@ -523,7 +591,7 @@
</product>
</function>
<function name="aero/moment/Roll_left_spoiler">
<function name="aero/coefficient/Cldsp_l">
<description>Roll moment due to left spoiler</description>
<product>
<property>aero/qbar-psf</property>
@ -534,7 +602,7 @@
</product>
</function>
<function name="aero/moment/Roll_right_spoiler">
<function name="aero/coefficient/Cldsp_r">
<description>Roll moment due to right spoiler</description>
<product>
<property>aero/qbar-psf</property>
@ -545,14 +613,14 @@
</product>
</function>
<function name="aero/moment/Roll_rudder">
<function name="aero/coefficient/Cldr">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
<value>0.01</value>
<value>0.008</value>
</product>
</function>
@ -560,18 +628,63 @@
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<function name="aero/coefficient/Cmalpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.5918</value>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-9.4468 0.1997
-6.3284 0.1313
-5.4416 0.1101
-4.3131 0.0870
-3.0234 0.0599
-2.0214 0.0359
-0.6629 0.0132
0.4655 -0.0090
1.6628 -0.0281
2.9406 -0.0455
4.0685 -0.0566
5.2651 -0.0624
6.3583 -0.0698
7.3937 -0.0718
8.5212 -0.0736
9.8677 -0.0851
11.3179 -0.1017
20.1549 -0.2027
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_left_elevator">
<function name="aero/coefficient/Cmq">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-28.9</value>
</product>
</function>
<function name="aero/coefficient/Cmadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-0.94671</value>
</product>
</function>
<function name="aero/coefficient/Cmde_l">
<description>Pitch moment due to left elevator</description>
<product>
<property>aero/qbar-psf</property>
@ -582,7 +695,7 @@
</product>
</function>
<function name="aero/moment/Pitch_right_elevator">
<function name="aero/coefficient/Cmde_r">
<description>Pitch moment due to right elevator</description>
<product>
<property>aero/qbar-psf</property>
@ -593,38 +706,14 @@
</product>
</function>
<function name="aero/moment/Pitch_elevator_trim">
<description>Pitch moment due to elevator trim control</description>
<function name="aero/coefficient/Cmdstab">
<description>Pitch moment due to stabilizer</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<toradians><property>hydraulics/elevator-trim/final-deg</property></toradians>
<value>-2.22479</value>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-37.4</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1.0356</value>
<toradians><property>hydraulics/stabilizer/final-deg</property></toradians>
<value>-1.975</value>
</product>
</function>
@ -632,18 +721,29 @@
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<function name="aero/coefficient/Cnbeta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.1292</value>
<property>aero/beta-deg</property>
<value>0.44</value>
<table>
<independentVar lookup="row">aero/alpha-deg</independentVar>
<tableData>
-4.7093 0.0045
-2.2164 0.0048
0.2903 0.0044
2.9836 0.0041
5.5629 0.0047
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<function name="aero/coefficient/Cnr">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
@ -655,14 +755,14 @@
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<function name="aero/coefficient/Cndr">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<toradians><property>hydraulics/rudder/final-deg</property></toradians>
<value>0.067</value>
<value>0.061</value>
</product>
</function>

12
Systems/a320-fcs.xml
View file

@ -306,7 +306,7 @@
<channel name="Pitch Trim">
<switch name="hydraulics/elevator-trim/rate">
<switch name="hydraulics/stabilizer/rate">
<default value="0.125"/>
<test logic="OR" value="0.25">
/systems/hydraulic/yellow-psi ge 1500
@ -314,7 +314,7 @@
</test>
</switch>
<aerosurface_scale name="hydraulics/elevator-trim/cmd-deg">
<aerosurface_scale name="hydraulics/stabilizer/cmd-deg">
<input>/controls/flight/elevator-trim</input>
<domain>
<min>-1.0</min>
@ -326,11 +326,11 @@
</range>
</aerosurface_scale>
<actuator name="hydraulics/elevator-trim/final-actuator">
<input>hydraulics/elevator-trim/cmd-deg</input>
<rate_limit>hydraulics/elevator-trim/rate</rate_limit>
<actuator name="hydraulics/stabilizer/final-actuator">
<input>hydraulics/stabilizer/cmd-deg</input>
<rate_limit>hydraulics/stabilizer/rate</rate_limit>
<lag>22.5</lag>
<output>hydraulics/elevator-trim/final-deg</output>
<output>hydraulics/stabilizer/final-deg</output>
</actuator>
</channel>

2
Systems/a320-ground-reactions.xml
View file

@ -4,6 +4,7 @@
<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
<ground_reactions>
<contact type="BOGEY" name="NOSE_LG">
<location unit="M">
<x>-13.6519</x>
@ -360,4 +361,5 @@
<brake_group>NONE</brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>

2
Systems/flight-recorder.xml
View file

@ -88,7 +88,7 @@
</signal>
<signal>
<type>float</type>
<property>/fdm/jsbsim/hydraulics/elevator-trim/final-deg</property>
<property>/fdm/jsbsim/hydraulics/stabilizer/final-deg</property>
</signal>
<signal>
<type>float</type>

2
Systems/lower-ecam.xml
View file

@ -179,7 +179,7 @@
<name>Elevator Trim Deg</name>
<type>gain</type>
<gain>-1.0</gain>
<input>/fdm/jsbsim/hydraulics/elevator-trim/final-deg</input>
<input>/fdm/jsbsim/hydraulics/stabilizer/final-deg</input>
<output>/ECAM/Lower/elevator-trim-deg</output>
</filter>