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fix FDE: Rudder, Lift/Drag, Flaps, Pulling Left, fix PFD flap overspeed tape

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This commit is contained in:
Joshua Davidson 2017-05-07 15:26:41 -04:00
parent 7068540458
commit 67df3fcb04
11 changed files with 238 additions and 301 deletions
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95
A319-100-IAE.xml
View file

@ -439,7 +439,7 @@ YAW MOI_________3950000______23089847_______24848934
<engine file="v2527_a5">
<location unit="IN">
<x> 620.00683 </x>
<x> 620.0683 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
@ -662,59 +662,14 @@ YAW MOI_________3950000______23089847_______24848934
<output>fcs/throttle-pos-norm[1]</output>
</pure_gain>
</channel>
<channel name="Yaw">
<!-- Testing on Ground steering Rudder bug
<pure_gain name="Yaw Damper Rate">
<input>velocities/r-rad_sec</input>
<gain>2</gain>
<pure_gain name="fcs/rudder-cmd">
<input>/controls/flight/rudder-fdm</input>
<gain>-1</gain>
<output>fcs/rudder-cmd-norm</output>
</pure_gain>
<pure_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<gain>-5</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<summer name="Rudder Sum">
<input>fcs/yaw-trim-sum</input>
<input>fcs/yaw-damper-rate</input>
<input>fcs/yaw-damper-beta</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<gain>0.01745</gain>
<range>
<min>-25</min>
<max>25</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder position normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-25</min>
<max>25</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
@ -960,10 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.780
0.00 0.335
0.23 1.090
0.60 0.690
-0.20 -0.520
0.00 0.505
0.23 1.800
0.60 1.000
</tableData>
</table>
</product>
@ -974,8 +929,16 @@ YAW MOI_________3950000______23089847_______24848934
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00700 </value>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00350
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
@ -985,7 +948,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.02500 </value>
<value> 0.01000 </value>
</product>
</function>
@ -995,7 +958,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.1</value>
<value>-0.15</value>
</product>
</function>
@ -1024,8 +987,8 @@ YAW MOI_________3950000______23089847_______24848934
-1.57 1.300
-0.26 0.021
0.00 0.012
0.26 0.021
1.57 1.300
0.26 0.028
1.57 1.350
</tableData>
</table>
</product>
@ -1074,7 +1037,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
<value> 0.00200 </value>
</product>
</function>
@ -1084,7 +1047,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.020</value>
<value>0.030</value>
</product>
</function>
@ -1094,7 +1057,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.02</value>
<value>0.03</value>
</product>
</function>
@ -1280,7 +1243,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.15</value>
<value>-0.2</value>
</product>
</function>
@ -1291,7 +1254,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.1</value>
<value>-0.2</value>
</product>
</function>

95
A320-200-IAE.xml
View file

@ -439,7 +439,7 @@ YAW MOI_________3950000______23089847_______24848934
<engine file="v2527_a5">
<location unit="IN">
<x> 620.00683 </x>
<x> 620.0683 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
@ -662,59 +662,14 @@ YAW MOI_________3950000______23089847_______24848934
<output>fcs/throttle-pos-norm[1]</output>
</pure_gain>
</channel>
<channel name="Yaw">
<!-- Testing on Ground steering Rudder bug
<pure_gain name="Yaw Damper Rate">
<input>velocities/r-rad_sec</input>
<gain>2</gain>
<pure_gain name="fcs/rudder-cmd">
<input>/controls/flight/rudder-fdm</input>
<gain>-1</gain>
<output>fcs/rudder-cmd-norm</output>
</pure_gain>
<pure_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<gain>-5</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<summer name="Rudder Sum">
<input>fcs/yaw-trim-sum</input>
<input>fcs/yaw-damper-rate</input>
<input>fcs/yaw-damper-beta</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<gain>0.01745</gain>
<range>
<min>-25</min>
<max>25</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder position normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-25</min>
<max>25</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
@ -960,10 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.780
0.00 0.335
0.23 1.090
0.60 0.690
-0.20 -0.520
0.00 0.505
0.23 1.800
0.60 1.000
</tableData>
</table>
</product>
@ -974,8 +929,16 @@ YAW MOI_________3950000______23089847_______24848934
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00700 </value>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00350
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
@ -985,7 +948,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.02500 </value>
<value> 0.01000 </value>
</product>
</function>
@ -995,7 +958,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.1</value>
<value>-0.15</value>
</product>
</function>
@ -1024,8 +987,8 @@ YAW MOI_________3950000______23089847_______24848934
-1.57 1.300
-0.26 0.021
0.00 0.012
0.26 0.021
1.57 1.300
0.26 0.028
1.57 1.350
</tableData>
</table>
</product>
@ -1074,7 +1037,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
<value> 0.00200 </value>
</product>
</function>
@ -1084,7 +1047,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.020</value>
<value>0.030</value>
</product>
</function>
@ -1094,7 +1057,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.02</value>
<value>0.03</value>
</product>
</function>
@ -1280,7 +1243,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.15</value>
<value>-0.2</value>
</product>
</function>
@ -1291,7 +1254,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.1</value>
<value>-0.2</value>
</product>
</function>

12
A320-main.xml
View file

@ -280,8 +280,8 @@
<config>
<altitude-dial-mode>0</altitude-dial-mode>
<roll>
<umin>-0.40</umin>
<umax>0.40</umax>
<umin>-0.55</umin>
<umax>0.55</umax>
<kp>0.05</kp>
<kp-vloc>0.07</kp-vloc>
<ti>10.0</ti>
@ -297,8 +297,8 @@
<kp-cws>-0.09</kp-cws>
</pitch>
<cmd>
<roll-kp>-1.0</roll-kp>
<roll-scale>1.4</roll-scale>
<roll-kp>-0.9</roll-kp>
<roll-scale>1.6</roll-scale>
<vorloc>-4.0</vorloc>
<alt>0.025</alt>
<vs>0.05</vs>
@ -309,7 +309,7 @@
<autoland>
<kp-roll>0.10</kp-roll>
<kp-pitch>0.05</kp-pitch>
<kp-rudder>-0.3</kp-rudder>
<kp-rudder>-0.1</kp-rudder>
</autoland>
</config>
<settings>
@ -321,7 +321,7 @@
<retard-ft>40</retard-ft> <!-- Enable Thrust Retard -->
<retard-enable>0</retard-enable> <!-- AGL to Thrust Retard -->
<togaspd>162</togaspd> <!-- V2 + 10kts -->
<lat-agl-ft>100</lat-agl-ft> <!-- Set to 999999 if you do not want T/O to change automatically to HDG, or LNAV -->
<lat-agl-ft>30</lat-agl-ft> <!-- Set to 999999 if you do not want T/O to change automatically to HDG, or LNAV -->
<reduc-agl-ft>1450</reduc-agl-ft> <!-- Set to 999999 if you do not want TOGA to change automatically to FLCH -->
</settings>
<output>

95
A321-200-IAE.xml
View file

@ -439,7 +439,7 @@ YAW MOI_________3950000______23089847_______24848934
<engine file="v2533_a5">
<location unit="IN">
<x> 620.00683 </x>
<x> 620.0683 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
@ -662,59 +662,14 @@ YAW MOI_________3950000______23089847_______24848934
<output>fcs/throttle-pos-norm[1]</output>
</pure_gain>
</channel>
<channel name="Yaw">
<!-- Testing on Ground steering Rudder bug
<pure_gain name="Yaw Damper Rate">
<input>velocities/r-rad_sec</input>
<gain>2</gain>
<pure_gain name="fcs/rudder-cmd">
<input>/controls/flight/rudder-fdm</input>
<gain>-1</gain>
<output>fcs/rudder-cmd-norm</output>
</pure_gain>
<pure_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<gain>-5</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<summer name="Rudder Sum">
<input>fcs/yaw-trim-sum</input>
<input>fcs/yaw-damper-rate</input>
<input>fcs/yaw-damper-beta</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<gain>0.01745</gain>
<range>
<min>-25</min>
<max>25</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder position normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-25</min>
<max>25</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
@ -960,10 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.780
0.00 0.335
0.23 1.090
0.60 0.690
-0.20 -0.520
0.00 0.505
0.23 1.800
0.60 1.000
</tableData>
</table>
</product>
@ -974,8 +929,16 @@ YAW MOI_________3950000______23089847_______24848934
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00700 </value>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00350
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
@ -985,7 +948,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.02500 </value>
<value> 0.01000 </value>
</product>
</function>
@ -995,7 +958,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.1</value>
<value>-0.15</value>
</product>
</function>
@ -1024,8 +987,8 @@ YAW MOI_________3950000______23089847_______24848934
-1.57 1.300
-0.26 0.021
0.00 0.012
0.26 0.021
1.57 1.300
0.26 0.028
1.57 1.350
</tableData>
</table>
</product>
@ -1074,7 +1037,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
<value> 0.00200 </value>
</product>
</function>
@ -1084,7 +1047,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.020</value>
<value>0.030</value>
</product>
</function>
@ -1094,7 +1057,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.02</value>
<value>0.03</value>
</product>
</function>
@ -1280,7 +1243,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.15</value>
<value>-0.2</value>
</product>
</function>
@ -1291,7 +1254,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.1</value>
<value>-0.2</value>
</product>
</function>

95
ACJ-IAE.xml
View file

@ -439,7 +439,7 @@ YAW MOI_________3950000______23089847_______24848934
<engine file="v2527_a5">
<location unit="IN">
<x> 620.00683 </x>
<x> 620.0683 </x>
<y> 226.575 </y>
<z> -45.567 </z>
</location>
@ -662,59 +662,14 @@ YAW MOI_________3950000______23089847_______24848934
<output>fcs/throttle-pos-norm[1]</output>
</pure_gain>
</channel>
<channel name="Yaw">
<!-- Testing on Ground steering Rudder bug
<pure_gain name="Yaw Damper Rate">
<input>velocities/r-rad_sec</input>
<gain>2</gain>
<pure_gain name="fcs/rudder-cmd">
<input>/controls/flight/rudder-fdm</input>
<gain>-1</gain>
<output>fcs/rudder-cmd-norm</output>
</pure_gain>
<pure_gain name="Yaw Damper Beta">
<input>aero/beta-rad</input>
<gain>-5</gain>
</pure_gain>
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<summer name="Rudder Sum">
<input>fcs/yaw-trim-sum</input>
<input>fcs/yaw-damper-rate</input>
<input>fcs/yaw-damper-beta</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/rudder-sum</input>
<gain>0.01745</gain>
<range>
<min>-25</min>
<max>25</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder position normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-25</min>
<max>25</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale> -->
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
@ -960,10 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.780
0.00 0.335
0.23 1.090
0.60 0.690
-0.20 -0.520
0.00 0.505
0.23 1.800
0.60 1.000
</tableData>
</table>
</product>
@ -974,8 +929,16 @@ YAW MOI_________3950000______23089847_______24848934
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00700 </value>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00350
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
@ -985,7 +948,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.02500 </value>
<value> 0.01000 </value>
</product>
</function>
@ -995,7 +958,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.1</value>
<value>-0.15</value>
</product>
</function>
@ -1024,8 +987,8 @@ YAW MOI_________3950000______23089847_______24848934
-1.57 1.300
-0.26 0.021
0.00 0.012
0.26 0.021
1.57 1.300
0.26 0.028
1.57 1.350
</tableData>
</table>
</product>
@ -1074,7 +1037,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
<value> 0.00200 </value>
</product>
</function>
@ -1084,7 +1047,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.020</value>
<value>0.030</value>
</product>
</function>
@ -1094,7 +1057,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.02</value>
<value>0.03</value>
</product>
</function>
@ -1280,7 +1243,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.15</value>
<value>-0.2</value>
</product>
</function>
@ -1291,7 +1254,7 @@ YAW MOI_________3950000______23089847_______24848934
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.1</value>
<value>-0.2</value>
</product>
</function>

7
AircraftConfig/acconfig.nas
View file

@ -30,6 +30,8 @@ var colddark = func {
setprop("/controls/flight/slats", 0.000);
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/flap-lever", 0);
setprop("/controls/flight/flap-pos", 0);
setprop("/controls/flight/flap-txt", " ");
setprop("/controls/flight/speedbrake-arm", 0);
setprop("/controls/gear/gear-down", 1);
systems.elec_init();
@ -74,6 +76,8 @@ var beforestart = func {
setprop("/controls/flight/slats", 0.000);
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/flap-lever", 0);
setprop("/controls/flight/flap-pos", 0);
setprop("/controls/flight/flap-txt", " ");
setprop("/controls/flight/speedbrake-arm", 0);
setprop("/controls/gear/gear-down", 1);
systems.elec_init();
@ -142,6 +146,8 @@ var taxi = func {
setprop("/controls/flight/slats", 0.000);
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/flap-lever", 0);
setprop("/controls/flight/flap-pos", 0);
setprop("/controls/flight/flap-txt", " ");
setprop("/controls/flight/speedbrake-arm", 0);
setprop("/controls/gear/gear-down", 1);
systems.elec_init();
@ -238,6 +244,7 @@ var takeoff = func {
setprop("/controls/flight/flaps", 0.290);
setprop("/controls/flight/slats", 0.666);
setprop("/controls/flight/flap-lever", 1);
setprop("/controls/flight/flap-pos", 2);
setprop("/controls/flight/flap-txt", "1+F");
setprop("/controls/flight/elevator-trim", -0.15);
}

45
Models/Instruments/PFD/PFD1.xml
View file

@ -119,10 +119,20 @@
<object-name>fd_roll</object-name>
<object-name>fd_pitch</object-name>
<condition>
<and>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<less-than>
<property>orientation/roll-deg</property>
<value>45</value>
</less-than>
<greater-than>
<property>orientation/roll-deg</property>
<value>-45</value>
</greater-than>
</and>
</condition>
</animation>
@ -255,7 +265,29 @@
<transform>
<subtype>textranslate</subtype>
<property>instrumentation/airspeed-indicator/indicated-speed-kt</property>
<factor>0.002001953</factor>
<interpolation>
<entry><ind> 0</ind><dep> 0</dep></entry>
<entry><ind> 20</ind><dep>0.040</dep></entry>
<entry><ind> 40</ind><dep>0.080</dep></entry>
<entry><ind> 60</ind><dep>0.118</dep></entry>
<entry><ind> 80</ind><dep>0.158</dep></entry>
<entry><ind>100</ind><dep>0.198</dep></entry>
<entry><ind>120</ind><dep>0.236</dep></entry>
<entry><ind>140</ind><dep>0.276</dep></entry>
<entry><ind>160</ind><dep>0.316</dep></entry>
<entry><ind>180</ind><dep>0.356</dep></entry>
<entry><ind>200</ind><dep>0.395</dep></entry>
<entry><ind>220</ind><dep>0.435</dep></entry>
<entry><ind>240</ind><dep>0.474</dep></entry>
<entry><ind>260</ind><dep>0.514</dep></entry>
<entry><ind>280</ind><dep>0.554</dep></entry>
<entry><ind>300</ind><dep>0.593</dep></entry>
<entry><ind>320</ind><dep>0.633</dep></entry>
<entry><ind>340</ind><dep>0.672</dep></entry>
<entry><ind>360</ind><dep>0.712</dep></entry>
<entry><ind>380</ind><dep>0.751</dep></entry>
<entry><ind>400</ind><dep>0.791</dep></entry>
</interpolation>
<axis>
<x>0</x>
<y>1</y>
@ -263,14 +295,15 @@
</axis>
</transform>
<transform>
<property>/controls/flight/flap-lever</property>
<property>/controls/flight/flap-pos</property>
<subtype>textranslate</subtype>
<interpolation>
<entry><ind>0</ind><dep>0</dep></entry>
<entry><ind>1</ind><dep>0.090625</dep></entry>
<entry><ind>2</ind><dep>0.1609375</dep></entry>
<entry><ind>3</ind><dep>0.23125</dep></entry>
<entry><ind>4</ind><dep>0.303984375</dep></entry>
<entry><ind>1</ind><dep>0.05</dep></entry>
<entry><ind>2</ind><dep>0.12</dep></entry>
<entry><ind>3</ind><dep>0.19</dep></entry>
<entry><ind>4</ind><dep>0.26</dep></entry>
<entry><ind>5</ind><dep>0.33</dep></entry>
</interpolation>
<axis>
<x>1</x>

45
Models/Instruments/PFD/PFD2.xml
View file

@ -119,10 +119,20 @@
<object-name>fd_roll</object-name>
<object-name>fd_pitch</object-name>
<condition>
<and>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
<less-than>
<property>orientation/roll-deg</property>
<value>45</value>
</less-than>
<greater-than>
<property>orientation/roll-deg</property>
<value>-45</value>
</greater-than>
</and>
</condition>
</animation>
@ -255,7 +265,29 @@
<transform>
<subtype>textranslate</subtype>
<property>instrumentation/airspeed-indicator/indicated-speed-kt</property>
<factor>0.002001953</factor>
<interpolation>
<entry><ind> 0</ind><dep> 0</dep></entry>
<entry><ind> 20</ind><dep>0.040</dep></entry>
<entry><ind> 40</ind><dep>0.080</dep></entry>
<entry><ind> 60</ind><dep>0.118</dep></entry>
<entry><ind> 80</ind><dep>0.158</dep></entry>
<entry><ind>100</ind><dep>0.198</dep></entry>
<entry><ind>120</ind><dep>0.236</dep></entry>
<entry><ind>140</ind><dep>0.276</dep></entry>
<entry><ind>160</ind><dep>0.316</dep></entry>
<entry><ind>180</ind><dep>0.356</dep></entry>
<entry><ind>200</ind><dep>0.395</dep></entry>
<entry><ind>220</ind><dep>0.435</dep></entry>
<entry><ind>240</ind><dep>0.474</dep></entry>
<entry><ind>260</ind><dep>0.514</dep></entry>
<entry><ind>280</ind><dep>0.554</dep></entry>
<entry><ind>300</ind><dep>0.593</dep></entry>
<entry><ind>320</ind><dep>0.633</dep></entry>
<entry><ind>340</ind><dep>0.672</dep></entry>
<entry><ind>360</ind><dep>0.712</dep></entry>
<entry><ind>380</ind><dep>0.751</dep></entry>
<entry><ind>400</ind><dep>0.791</dep></entry>
</interpolation>
<axis>
<x>0</x>
<y>1</y>
@ -263,14 +295,15 @@
</axis>
</transform>
<transform>
<property>/controls/flight/flap-lever</property>
<property>/controls/flight/flap-pos</property>
<subtype>textranslate</subtype>
<interpolation>
<entry><ind>0</ind><dep>0</dep></entry>
<entry><ind>1</ind><dep>0.090625</dep></entry>
<entry><ind>2</ind><dep>0.1609375</dep></entry>
<entry><ind>3</ind><dep>0.23125</dep></entry>
<entry><ind>4</ind><dep>0.303984375</dep></entry>
<entry><ind>1</ind><dep>0.05</dep></entry>
<entry><ind>2</ind><dep>0.12</dep></entry>
<entry><ind>3</ind><dep>0.19</dep></entry>
<entry><ind>4</ind><dep>0.26</dep></entry>
<entry><ind>5</ind><dep>0.33</dep></entry>
</interpolation>
<axis>
<x>1</x>

BIN
Models/Instruments/PFD/res/spd-tape.png
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11
Nasal/fctl.nas
View file

@ -2,6 +2,7 @@
# In air, flaps 1 is slats only. On ground, it is slats and flaps.
setprop("/controls/flight/flap-lever", 0);
setprop("/controls/flight/flap-pos", 0);
setprop("/controls/flight/flap-txt", " ");
controls.flapsDown = func(step) {
@ -11,12 +12,14 @@ controls.flapsDown = func(step) {
setprop("/controls/flight/flaps", 0.290);
setprop("/controls/flight/slats", 0.666);
setprop("/controls/flight/flap-lever", 1);
setprop("/controls/flight/flap-pos", 2);
setprop("/controls/flight/flap-txt", "1+F");
return;
} else {
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/slats", 0.666);
setprop("/controls/flight/flap-lever", 1);
setprop("/controls/flight/flap-pos", 1);
setprop("/controls/flight/flap-txt", "1");
return;
}
@ -24,18 +27,21 @@ controls.flapsDown = func(step) {
setprop("/controls/flight/flaps", 0.596);
setprop("/controls/flight/slats", 0.814);
setprop("/controls/flight/flap-lever", 2);
setprop("/controls/flight/flap-pos", 3);
setprop("/controls/flight/flap-txt", "2");
return;
} else if (getprop("/controls/flight/flap-lever") == 2) {
setprop("/controls/flight/flaps", 0.645);
setprop("/controls/flight/slats", 0.814);
setprop("/controls/flight/flap-lever", 3);
setprop("/controls/flight/flap-pos", 4);
setprop("/controls/flight/flap-txt", "3");
return;
} else if (getprop("/controls/flight/flap-lever") == 3) {
setprop("/controls/flight/flaps", 1.000);
setprop("/controls/flight/slats", 1.000);
setprop("/controls/flight/flap-lever", 4);
setprop("/controls/flight/flap-pos", 5);
setprop("/controls/flight/flap-txt", "FULL");
return;
}
@ -44,12 +50,14 @@ controls.flapsDown = func(step) {
setprop("/controls/flight/flaps", 0.645);
setprop("/controls/flight/slats", 0.814);
setprop("/controls/flight/flap-lever", 3);
setprop("/controls/flight/flap-pos", 4);
setprop("/controls/flight/flap-txt", "3");
return;
} else if (getprop("/controls/flight/flap-lever") == 3) {
setprop("/controls/flight/flaps", 0.596);
setprop("/controls/flight/slats", 0.814);
setprop("/controls/flight/flap-lever", 2);
setprop("/controls/flight/flap-pos", 3);
setprop("/controls/flight/flap-txt", "2");
return;
} else if (getprop("/controls/flight/flap-lever") == 2) {
@ -57,12 +65,14 @@ controls.flapsDown = func(step) {
setprop("/controls/flight/flaps", 0.290);
setprop("/controls/flight/slats", 0.666);
setprop("/controls/flight/flap-lever", 1);
setprop("/controls/flight/flap-pos", 2);
setprop("/controls/flight/flap-txt", "1+F");
return;
} else {
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/slats", 0.666);
setprop("/controls/flight/flap-lever", 1);
setprop("/controls/flight/flap-pos", 1);
setprop("/controls/flight/flap-txt", "1");
return;
}
@ -70,6 +80,7 @@ controls.flapsDown = func(step) {
setprop("/controls/flight/flaps", 0.000);
setprop("/controls/flight/slats", 0.000);
setprop("/controls/flight/flap-lever", 0);
setprop("/controls/flight/flap-pos", 0);
setprop("/controls/flight/flap-txt", " ");
return;
}

7
Nasal/it-fbw.nas
View file

@ -13,12 +13,13 @@ var update_loop = func {
if (ail > 0.4 or ail < -0.4) {
setprop("/it-fbw/roll-lim-max", "67");
setprop("/it-fbw/roll-lim-min", "-67");
} else {
} else if (ail < 0.05 and ail > -0.05) {
setprop("/it-fbw/roll-lim-max", "33");
setprop("/it-fbw/roll-lim-min", "-33");
if (getprop("/it-fbw/law") > 33) {
} else {
if (getprop("/it-fbw/roll-deg") > 33) {
setprop("/it-fbw/roll-deg", "33");
} else if (getprop("/it-fbw/law") < -33) {
} else if (getprop("/it-fbw/roll-deg") < -33) {
setprop("/it-fbw/roll-deg", "-33");
}
}