Remove the c172p, there will be an updated version shortly.
This commit is contained in:
ehofman
parent
d71f743d62
commit
2c8aaa35ee
22 changed files with 0 additions and 16448 deletions
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@ -1,12 +0,0 @@
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<?xml version="1.0"?>
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<FG_PISTON NAME="IO320">
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MINMP 6.5
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MAXMP 29.92
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DISPLACEMENT 320.0
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MAXHP 160.0
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CYCLES 2.0
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IDLERPM 550.0
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MAXTHROTTLE 1.0
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MINTHROTTLE 0.2
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</FG_PISTON>
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@ -1,61 +0,0 @@
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<?xml version="1.0"?>
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<FG_PROPELLER NAME="Fixed-Pitch 75-inch Two-Blade Propeller">
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IXX 1.67
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DIAMETER 75
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NUMBLADES 2
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MINPITCH 22
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MAXPITCH 22
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C_THRUST 25 1
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0.0 0.068
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0.1 0.068
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0.2 0.067
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0.3 0.066
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||||
0.4 0.064
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||||
0.5 0.061
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||||
0.6 0.057
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||||
0.7 0.050
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||||
0.8 0.040
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||||
0.9 0.029
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||||
1.0 0.019
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||||
1.1 0.008
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1.2 -0.001
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||||
1.3 -0.008
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||||
1.4 -0.019
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1.5 -0.029
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1.6 -0.040
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1.7 -0.050
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1.8 -0.057
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1.9 -0.061
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2.0 -0.064
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||||
2.1 -0.066
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2.2 -0.067
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2.3 -0.068
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5.0 -0.068
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C_POWER 26 1
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0.0 0.0580
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0.1 0.0620
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0.2 0.0600
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0.3 0.0580
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||||
0.4 0.0520
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||||
0.5 0.0450
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||||
0.6 0.0421
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0.7 0.0389
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0.8 0.0346
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0.9 0.0280
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1.0 0.0202
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1.1 0.0111
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1.2 0.0075
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1.3 0.0111
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1.4 0.0202
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1.5 0.0280
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1.6 0.0346
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1.7 0.0389
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1.8 0.0421
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1.9 0.0436
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2.0 0.0445
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2.1 0.0445
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2.2 0.0442
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2.3 0.0431
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2.4 0.0424
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5.0 0.0413
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</FG_PROPELLER>
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@ -1,684 +0,0 @@
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<?xml version="1.0"?>
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<!--
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Legacy 2D instruments and actions for the 3D C172P cockpit.
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-->
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<!DOCTYPE PropertyList>
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<PropertyList>
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<name>C172P 2D instruments.</name>
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<background>Aircraft/c172/Panels/Textures/transparent-bg.rgb</background>
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<w>1424</w>
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<h>488</h>
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<view-height>500</view-height>
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<instruments>
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<!-- labels -->
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<instrument include="/labels/labelbcn.xml">
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<name>labelbcn</name>
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<x>495</x>
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<y>-270</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- labels -->
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<instrument include="/labels/labelnav.xml">
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<name>labelnav</name>
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<x>458</x>
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<y>-270</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- labels -->
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<instrument include="/labels/labelpto.xml">
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<name>labelpto</name>
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<x>422</x>
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<y>-270</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- labels -->
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<instrument include="/labels/labelsto.xml">
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<name>labelsto</name>
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<x>525</x>
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<y>-270</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- labels -->
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<instrument include="/labels/labeltax.xml">
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<name>labeltax</name>
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<x>493</x>
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<y>-204</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- labels -->
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<instrument include="/labels/labellng.xml">
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<name>labellng</name>
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<x>525</x>
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<y>-204</y>
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<w>28</w>
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<h>26</h>
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</instrument>
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<!-- engine gauge cluster -->
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<instrument include="../../Instruments/clock.xml">
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<name>Chronometer</name>
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<x>162</x>
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<y>216</y>
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<w>74</w>
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<h>74</h>
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</instrument>
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<instrument include="../../Instruments/egt.xml">
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<name>Exhaust Gas Temperature Gauge</name>
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<x>162</x>
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<y>142</y>
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<w>74</w>
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<h>74</h>
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</instrument>
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<instrument include="../../Instruments/fuel.xml">
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<name>Fuel Gauge</name>
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<x>85</x>
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<y>142</y>
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<w>74</w>
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<h>74</h>
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</instrument>
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<instrument include="../../Instruments/oil.xml">
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<name>Oil Gauge</name>
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<x>85</x>
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<y>65</y>
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<w>74</w>
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<h>74</h>
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</instrument>
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<instrument include="../../Instruments/vacamp.xml">
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<name>Vacuum Pressure Gauge</name>
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<x>162</x>
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<y>65</y>
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<w>74</w>
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<h>74</h>
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</instrument>
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<!-- end engine gauges cluster -->
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<!-- engine controls cluster -->
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<instrument include="../../Instruments/rpm.xml">
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<name>RPM Gauge</name>c172p-2d-panel.xml
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<x>496</x>
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<y>-25</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/single-magneto-switch.xml">
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<name>Magneto switch panel</name>
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<x>120</x>
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<y>-180</y>
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</instrument>
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<!-- end engine controls cluster -->
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<!-- sacred six -->
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<instrument include="../../Instruments/asi-160-knot.xml">
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<name>Airspeed Indicator</name>
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<x>264</x>
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<y>235</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/attitude-indicator.xml">
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<name>Attitude Gyro</name>
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<x>380</x>
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<y>235</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/altimeter.xml">
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<name>Altimeter</name>
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<x>496</x>
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<y>235</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/turn.xml">
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<name>Turn Coordinator</name>
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<x>264</x>
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<y>100</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/gyro.xml">
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<name>Directional Gyro</name>
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<x>380</x>
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<y>100</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/vertical.xml">
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<name>Vertical Velocity Indicator</name>
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<x>496</x>
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<y>100</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<!-- end sacred six -->
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<!-- radio nav instruments -->
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<instrument include="../../Instruments/nav1.xml">
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<name>VOR 1 Gauge</name>
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<x>620</x>
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<y>235</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/nav1.xml">
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<name>VOR 2 Gauge</name>
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<params>
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<nav-to-flag>/instrumentation/nav[1]/to-flag</nav-to-flag>
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<nav-from-flag>/instrumentation/nav[1]/from-flag</nav-from-flag>
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<nav-radial-selected>/instrumentation/nav[1]/radials/selected-deg</nav-radial-selected>
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<nav-gs-needle-deflection>/instrumentation/nav[1]/gs-needle-deflection</nav-gs-needle-deflection>
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<nav-heading-needle-deflection>/instrumentation/nav[1]/heading-needle-deflection</nav-heading-needle-deflection>
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<nav-has-gs-needle>/sim/instrument-options/nav[1]/has-gs-needle</nav-has-gs-needle>
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<nav-needles-pivot>/sim/instrument-options/nav[1]/needles-pivot</nav-needles-pivot>
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</params>
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<x>620</x>
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<y>100</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<instrument include="../../Instruments/adf.xml">
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<name>ADF Gauge</name>
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<x>620</x>
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<y>-25</y>
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<w>115</w>
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<h>115</h>
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</instrument>
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<!-- end radio nav instruments -->
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<!-- radio stack -->
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<instrument include="../../Instruments/markerbeacon.xml">
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<name>Marker Beacon Indicators</name>
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<x>770</x>
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<y>290</y>
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</instrument>
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<instrument include="../../Instruments/navcom-radio.xml">
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<name>NavCom 1 Radio</name>
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<x>825</x>
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<y>240</y>
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<w>235</w>
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<h>60</h>
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</instrument>
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<instrument include="../../Instruments/navcom-radio.xml">
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<name>NavCom 2 Radio</name>
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<params>
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<comm-freq-selected-prop>/instrumentation/comm[1]/frequencies/selected-mhz</comm-freq-selected-prop>
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<comm-freq-standby-prop>/instrumentation/comm[1]/frequencies/standby-mhz</comm-freq-standby-prop>
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<nav-freq-selected-prop>/instrumentation/nav[1]/frequencies/selected-mhz</nav-freq-selected-prop>
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<nav-freq-standby-prop>/instrumentation/nav[1]/frequencies/standby-mhz</nav-freq-standby-prop>
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<nav-morse-id-volume-prop>/instrumentation/nav[1]/volume</nav-morse-id-volume-prop>
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<nav-morse-ident-toggle-prop>/instrumentation/nav[1]/ident</nav-morse-ident-toggle-prop>
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</params>
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<x>825</x>
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<y>180</y>
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<w>235</w>
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<h>60</h>
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</instrument>
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<instrument include="../../Instruments/adf-radio.xml">
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<name>ADF Radio</name>
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<x>825</x>
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<y>120</y>
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<w>235</w>
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<h>60</h>
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</instrument>
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<instrument include="../../Instruments/dme.xml">
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<name>DME</name>
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<x>825</x>
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<y>-50</y>
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</instrument>
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<!--
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<instrument include="../../Instruments/autopilot.xml">
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<name>Autopilot</name>
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<x>880</x>
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<y>-20</y>
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</instrument>
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-->
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<instrument include="../../Instruments/KAP140TwoAxisAlt.xml">
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<name>KAP140 Autopilot</name>
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<x>825</x>
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<y>60</y>
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<w>235</w>
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<h>60</h>
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</instrument>
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<!-- end radio stack -->
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<instrument>
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<name>3D Action Placeholder</name>
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<x>712</x>
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<y>0</y>
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<w>1424</w>
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<h>1488</h>
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<w-base>1424</w-base>
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<h-base>1488</h-base>
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<layers>
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<layer>
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<name>background</name>
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<texture>
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<path>Aircraft/c172/Panels/Textures/transparent-bg.rgb</path>
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||||
<x1>0.0</x1>
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||||
<y1>0.0</y1>
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||||
<x2>1.0</x2>
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<y2>1.0</y2>
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</texture>
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</layer>
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<layer>
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<name>background</name>
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<texture>
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<path>Aircraft/c172/Panels/Textures/transparent-bg.rgb</path>
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||||
<x1>0.0</x1>
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||||
<y1>0.0</y1>
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||||
<x2>1.0</x2>
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||||
<y2>1.0</y2>
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||||
</texture>
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</layer>
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<layer>
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<name>background</name>
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<texture>
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<path>Aircraft/c172/Panels/Textures/transparent-bg.rgb</path>
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||||
<x1>0.0</x1>
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||||
<y1>0.0</y1>
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||||
<x2>1.0</x2>
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||||
<y2>1.0</y2>
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||||
</texture>
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||||
</layer>
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<layer>
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<name>background</name>
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||||
<texture>
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||||
<path>Aircraft/c172/Panels/Textures/transparent-bg.rgb</path>
|
||||
<x1>0.0</x1>
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||||
<y1>0.0</y1>
|
||||
<x2>1.0</x2>
|
||||
<y2>1.0</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
<layer>
|
||||
<name>background</name>
|
||||
<texture>
|
||||
<path>Aircraft/c172/Panels/Textures/transparent-bg.rgb</path>
|
||||
<x1>0.0</x1>
|
||||
<y1>0.0</y1>
|
||||
<x2>1.0</x2>
|
||||
<y2>1.0</y2>
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||||
</texture>
|
||||
</layer>
|
||||
</layers>
|
||||
|
||||
<!-- toggle switches -->
|
||||
|
||||
<actions>
|
||||
<action>
|
||||
<name>toggle nav lights</name>
|
||||
<button>0</button>
|
||||
<x>-267</x>
|
||||
<y>-246</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/lighting/nav-lights</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>toggle beacon light </name>
|
||||
<button>0</button>
|
||||
<x>-233</x>
|
||||
<y>-246</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/lighting/beacon</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>toggle pitot heat</name>
|
||||
<button>0</button>
|
||||
<x>-307</x>
|
||||
<y>-246</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/anti-ice/pitot-heat</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
|
||||
<action>
|
||||
<name>toggle strobe light</name>
|
||||
<button>0</button>
|
||||
<x>-198</x>
|
||||
<y>-246</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/lighting/strobe</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>toggle taxi light</name>
|
||||
<button>0</button>
|
||||
<x>-230</x>
|
||||
<y>-180</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/lighting/taxi-light</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>toggle landing light</name>
|
||||
<button>0</button>
|
||||
<x>-198</x>
|
||||
<y>-180</y>
|
||||
<w>20</w>
|
||||
<h>50</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/lighting/landing-lights</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<!-- elevator-trim -->
|
||||
|
||||
|
||||
<action>
|
||||
<name>small increase</name>
|
||||
<button>0</button>
|
||||
<x>-90</x>
|
||||
<y>-470</y>
|
||||
<w>60</w>
|
||||
<h>110</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/flight/elevator-trim</property>
|
||||
<step>0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>small decrease</name>
|
||||
<button>0</button>
|
||||
<x>-90</x>
|
||||
<y>-580</y>
|
||||
<w>60</w>
|
||||
<h>110</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/flight/elevator-trim</property>
|
||||
<step>-0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
|
||||
|
||||
<!-- flap extend/retract -->
|
||||
<action>
|
||||
<name>Flap Retract</name>
|
||||
<button>0</button>
|
||||
<x>230</x>
|
||||
<y>-245</y>
|
||||
<w>30</w>
|
||||
<h>80</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/flight/flaps</property>
|
||||
<step>-0.34</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>Flap Extend</name>
|
||||
<button>0</button>
|
||||
<x>260</x>
|
||||
<y>-245</y>
|
||||
<w>30</w>
|
||||
<h>80</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/flight/flaps</property>
|
||||
<step>0.34</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<!-- carb heat control -->
|
||||
|
||||
<action>
|
||||
<desc>carb-heat</desc>
|
||||
<button>0</button>
|
||||
<x>-145</x>
|
||||
<y>-240</y>
|
||||
<w>55</w>
|
||||
<h>95</h>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>controls/anti-ice/engine/carb-heat</property>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
|
||||
|
||||
|
||||
<!-- throttle control -->
|
||||
|
||||
<action>
|
||||
<name>big decrease</name>
|
||||
<button>0</button>
|
||||
<x>-45</x>
|
||||
<y>-215</y>
|
||||
<w>45</w>
|
||||
<h>90</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/throttle</property>
|
||||
<step>-0.07</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>big increase</name>
|
||||
<button>0</button>
|
||||
<x>0</x>
|
||||
<y>-215</y>
|
||||
<w>45</w>
|
||||
<h>90</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/throttle</property>
|
||||
<step>0.07</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>big decrease</name>
|
||||
<button>0</button>
|
||||
<x>-30</x>
|
||||
<y>-315</y>
|
||||
<w>45</w>
|
||||
<h>100</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/throttle</property>
|
||||
<step>-0.07</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>big increase</name>
|
||||
<button>0</button>
|
||||
<x>15</x>
|
||||
<y>-315</y>
|
||||
<w>50</w>
|
||||
<h>100</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/throttle</property>
|
||||
<step>0.07</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
<!-- mixture control -->
|
||||
|
||||
<action>
|
||||
<name>small decrease</name>
|
||||
<button>0</button>
|
||||
<x>80</x>
|
||||
<y>-215</y>
|
||||
<w>45</w>
|
||||
<h>90</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/mixture</property>
|
||||
<step>-0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>c172p-2d-panel.xml
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>small increase</name>
|
||||
<button>0</button>
|
||||
<x>125</x>
|
||||
<y>-215</y>
|
||||
<w>45</w>
|
||||
<h>90</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/mixture</property>
|
||||
<step>0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
|
||||
<action>
|
||||
<name>small decrease</name>
|
||||
<button>0</button>
|
||||
<x>110</x>
|
||||
<y>-315</y>
|
||||
<w>50</w>
|
||||
<h>100</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/mixture</property>
|
||||
<step>-0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>c172p-2d-panel.xml
|
||||
</action>
|
||||
|
||||
<action>
|
||||
<name>small increase</name>
|
||||
<button>0</button>
|
||||
<x>160</x>
|
||||
<y>-315</y>
|
||||
<w>50</w>
|
||||
<h>100</h>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>controls/engines/engine/mixture</property>
|
||||
<step>0.03</step>
|
||||
<min>0</min>
|
||||
<max>1.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
|
||||
</actions>
|
||||
|
||||
</instrument>
|
||||
|
||||
</instruments>
|
||||
|
||||
</PropertyList>
|
||||
|
||||
|
||||
Binary file not shown.
Binary file not shown.
File diff suppressed because it is too large
Load diff
|
|
@ -1,675 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<path>c172p.ac</path>
|
||||
|
||||
<!-- Temporarily use the 2D panel hack, until I have time to make
|
||||
3D instruments -->
|
||||
|
||||
<panel>
|
||||
<!-- <name>PanelInstruments</name> -->
|
||||
<path>Aircraft/c172p/Models/c172p-2d-panel.xml</path>
|
||||
<bottom-left>
|
||||
<x-m>-0.37</x-m>
|
||||
<y-m>-0.50</y-m>
|
||||
<z-m>-0.10</z-m>
|
||||
</bottom-left>
|
||||
<bottom-right>
|
||||
<x-m>-0.37</x-m>
|
||||
<y-m> 0.50</y-m>
|
||||
<z-m>-0.10</z-m>
|
||||
</bottom-right>
|
||||
<top-left>
|
||||
<x-m>-0.37</x-m>
|
||||
<y-m>-0.50</y-m>
|
||||
<z-m> 0.25</z-m>
|
||||
</top-left>
|
||||
</panel>
|
||||
|
||||
<model>
|
||||
<name>MagCompass</name>
|
||||
<path>Aircraft/Instruments-3d/mag-compass.xml</path>
|
||||
<offsets>
|
||||
<x-m>-0.35</x-m>
|
||||
<y-m>0.00</y-m>
|
||||
<z-m>0.16</z-m>
|
||||
</offsets>
|
||||
</model>
|
||||
|
||||
<!-- LOD for the model as a whole -->
|
||||
|
||||
<animation>
|
||||
<type>range</type>
|
||||
<min-m>0</min-m>
|
||||
<max-m>10000</max-m>
|
||||
</animation>
|
||||
|
||||
<!-- Controls -->
|
||||
|
||||
|
||||
<animation>
|
||||
<name>CarbHeatGroup</name>
|
||||
<object-name>CarbHeat</object-name>
|
||||
<object-name>CarbHeatBack</object-name>
|
||||
<object-name>CarbHeatRod</object-name>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<name>ThrottleGroup</name>
|
||||
<object-name>Throttle</object-name>
|
||||
<object-name>ThrottleRod</object-name>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<name>MixtureGroup</name>
|
||||
<object-name>Mixture</object-name>
|
||||
<object-name>MixtureRod</object-name>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<name>FlapSwitchGroup</name>
|
||||
<object-name>FlapSwitch</object-name>
|
||||
<object-name>FlapSwitchRod</object-name>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<name>ElectronicsGroup</name>
|
||||
<object-name>TaxiLightSwitch</object-name>
|
||||
<object-name>LandingLightSwitch</object-name>
|
||||
<object-name>PitotHeatSwitch</object-name>
|
||||
<object-name>NavLightSwitch</object-name>
|
||||
<object-name>BeaconSwitch</object-name>
|
||||
<object-name>StrobeSwitch</object-name>
|
||||
<!--
|
||||
<object-name>ElectronicsLabels</object-name>
|
||||
<object-name>ElectronicsLabels2</object-name>
|
||||
-->
|
||||
</animation>
|
||||
|
||||
<!-- <animation>
|
||||
<name>ControlsGroup</name>
|
||||
<object-name>PanelInstruments</object-name>
|
||||
<object-name>ElectronicsGroup</object-name>
|
||||
<object-name>LeftYoke</object-name>
|
||||
<object-name>RightYoke</object-name>
|
||||
<object-name>CarbHeatGroup</object-name>
|
||||
<object-name>ThrottleGroup</object-name>
|
||||
<object-name>MixtureGroup</object-name>
|
||||
<object-name>FlapSwitchGroup</object-name>
|
||||
<object-name>TrimWheel</object-name>
|
||||
</animation> -->
|
||||
|
||||
<!-- <animation>
|
||||
<type>range</type>
|
||||
<object-name>ControlsGroup</object-name>
|
||||
<min-m>0</min-m>
|
||||
<max-m>10.0</max-m>
|
||||
</animation> -->
|
||||
|
||||
<animation>
|
||||
<type>translate</type>
|
||||
<object-name>LeftYoke</object-name>
|
||||
<object-name>RightYoke</object-name>
|
||||
<property>controls/flight/elevator</property>
|
||||
<factor>-0.03</factor>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>LeftYoke</object-name>
|
||||
<property>controls/flight/aileron</property>
|
||||
<factor>-45</factor>
|
||||
<center>
|
||||
<x-m>-0.23</x-m>
|
||||
<y-m>-0.245</y-m>
|
||||
<z-m>-0.13</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>RightYoke</object-name>
|
||||
<property>controls/flight/aileron</property>
|
||||
<factor>-45</factor>
|
||||
<center>
|
||||
<x-m>-0.23</x-m>
|
||||
<y-m>0.245</y-m>
|
||||
<z-m>-0.13</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>translate</type>
|
||||
<object-name>CarbHeatGroup</object-name>
|
||||
<property>controls/anti-ice/engine[0]/carb-heat</property>
|
||||
<factor>-0.04</factor>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>translate</type>
|
||||
<object-name>ThrottleGroup</object-name>
|
||||
<property>controls/engines/engine[0]/throttle</property>
|
||||
<factor>-0.10</factor>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>translate</type>
|
||||
<object-name>MixtureGroup</object-name>
|
||||
<property>controls/engines/engine[0]/mixture</property>
|
||||
<factor>-0.10</factor>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<property>controls/flight/flaps</property>
|
||||
<object-name>FlapSwitchGroup</object-name>
|
||||
<factor>60</factor>
|
||||
<offset-deg>-30</offset-deg>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.39</x-m>
|
||||
<y-m>0.19</y-m>
|
||||
<z-m>-0.25</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>TrimWheel</object-name>
|
||||
<property>controls/flight/elevator-trim</property>
|
||||
<factor>-360</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.41</x-m>
|
||||
<y-m>-0.04</y-m>
|
||||
<z-m>-0.46</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>TaxiLightSwitch</object-name>
|
||||
<property>controls/lighting/taxi-light</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.221</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>LandingLightSwitch</object-name>
|
||||
<property>controls/lighting/landing-lights</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.221</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>PitotHeatSwitch</object-name>
|
||||
<property>controls/anti-ice/pitot-heat</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.269</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>NavLightSwitch</object-name>
|
||||
<property>controls/lighting/nav-lights</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.269</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>BeaconSwitch</object-name>
|
||||
<property>controls/lighting/beacon</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.269</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>StrobeSwitch</object-name>
|
||||
<property>controls/lighting/strobe</property>
|
||||
<factor>-55</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>-0.363</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.269</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
<!-- Interior -->
|
||||
|
||||
<animation>
|
||||
<name>InteriorGroup</name>
|
||||
<object-name>Cabin</object-name>
|
||||
<object-name>Panel</object-name>
|
||||
<object-name>PilotSeat</object-name>
|
||||
<object-name>CopilotSeat</object-name>
|
||||
<object-name>BackSeat</object-name>
|
||||
<object-name>MagCompass</object-name>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>range</type>
|
||||
<object-name>InteriorGroup</object-name>
|
||||
<min-m>0</min-m>
|
||||
<max-m>50</max-m>
|
||||
</animation>
|
||||
|
||||
<!-- Airframe -->
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>Propeller</object-name>
|
||||
<condition>
|
||||
<less-than>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<value>200</value>
|
||||
</less-than>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>Propeller.Slow</object-name>
|
||||
<condition>
|
||||
<and>
|
||||
<greater-than>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<value>190</value>
|
||||
</greater-than>
|
||||
<less-than>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<value>1200</value>
|
||||
</less-than>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>Propeller.Fast</object-name>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<value>1200</value>
|
||||
</greater-than>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>LeftNavLightOn</object-name>
|
||||
<object-name>RightNavLightOn</object-name>
|
||||
<object-name>RearNavLightOn</object-name>
|
||||
<condition>
|
||||
<property>controls/lighting/nav-lights</property>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>LeftNavLightOff</object-name>
|
||||
<object-name>RightNavLightOff</object-name>
|
||||
<object-name>RearNavLightOff</object-name>
|
||||
<condition>
|
||||
<not>
|
||||
<property>controls/lighting/nav-lights</property>
|
||||
</not>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<name>BeaconFlasher</name>
|
||||
<type>timed</type>
|
||||
<object-name>BeaconOff</object-name>
|
||||
<object-name>BeaconOn</object-name>
|
||||
<duration-sec>1.0</duration-sec>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>BeaconFlasher</object-name>
|
||||
<condition>
|
||||
<property>controls/lighting/beacon</property>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<!-- Experimental Taxi and Landing Lights -->
|
||||
|
||||
|
||||
<animation>
|
||||
<type>spin</type>
|
||||
<object-name>Propeller</object-name>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<factor>-1</factor>
|
||||
<center>
|
||||
<x-m>-1.77</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.12</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>spin</type>
|
||||
<object-name>Propeller.Slow</object-name>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<factor>-0.1</factor>
|
||||
<center>
|
||||
<x-m>-1.77</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.12</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>spin</type>
|
||||
<object-name>Propeller.Fast</object-name>
|
||||
<property>engines/engine[0]/rpm</property>
|
||||
<factor>-0.001</factor>
|
||||
<center>
|
||||
<x-m>-1.77</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.12</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>NoseWheel</object-name>
|
||||
<object-name>NoseWheelStrut</object-name>
|
||||
<object-name>Axle</object-name>
|
||||
<property>surface-positions/rudder-pos-norm</property>
|
||||
<factor>-30.0</factor>
|
||||
<center>
|
||||
<x-m>-0.9</x-m>
|
||||
<y-m>0</y-m>
|
||||
<z-m>-0.59</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.25</x>
|
||||
<y>0.00</y>
|
||||
<z>1.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>LeftAileron</object-name>
|
||||
<property>surface-positions/left-aileron-pos-norm</property>
|
||||
<interpolation>
|
||||
<entry>
|
||||
<ind>-1.0</ind>
|
||||
<dep>-15</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>0.0</ind>
|
||||
<dep>0</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>1.0</ind>
|
||||
<dep>20</dep>
|
||||
</entry>
|
||||
</interpolation>
|
||||
<center>
|
||||
<x-m>1.1</x-m>
|
||||
<y-m>-1.96</y-m>
|
||||
<z-m>0.35</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.49</x>
|
||||
<y>2.65</y>
|
||||
<z>-0.03</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>RightAileron</object-name>
|
||||
<property>surface-positions/right-aileron-pos-norm</property>
|
||||
<interpolation>
|
||||
<entry>
|
||||
<ind>-1.0</ind>
|
||||
<dep>20</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>0.0</ind>
|
||||
<dep>0</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>1.0</ind>
|
||||
<dep>-15</dep>
|
||||
</entry>
|
||||
</interpolation>
|
||||
<center>
|
||||
<x-m>1.1</x-m>
|
||||
<y-m>1.96</y-m>
|
||||
<z-m>0.35</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>-0.49</x>
|
||||
<y>2.65</y>
|
||||
<z>0.03</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>translate</type>
|
||||
<object-name>LeftFlap</object-name>
|
||||
<object-name>RightFlap</object-name>
|
||||
<property>surface-positions/flap-pos-norm</property>
|
||||
<factor>0.15</factor>
|
||||
<axis>
|
||||
<x>1.0</x>
|
||||
<y>0.0</y>
|
||||
<z>0.2</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>LeftFlap</object-name>
|
||||
<property>surface-positions/flap-pos-norm</property>
|
||||
<factor>30</factor>
|
||||
<center>
|
||||
<x-m>0.76</x-m>
|
||||
<y-m>-0.53</y-m>
|
||||
<z-m>0.32</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>-0.1</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>RightFlap</object-name>
|
||||
<property>surface-positions/flap-pos-norm</property>
|
||||
<factor>30</factor>
|
||||
<center>
|
||||
<x-m>0.76</x-m>
|
||||
<y-m>-0.53</y-m>
|
||||
<z-m>0.32</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.1</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>Elevators</object-name>
|
||||
<object-name>ElevatorTrimTab</object-name>
|
||||
<property>surface-positions/elevator-pos-norm</property>
|
||||
<interpolation>
|
||||
<entry>
|
||||
<ind>-1.0</ind>
|
||||
<dep>-28</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>0</ind>
|
||||
<dep>0</dep>
|
||||
</entry>
|
||||
<entry>
|
||||
<ind>1.0</ind>
|
||||
<dep>23</dep>
|
||||
</entry>
|
||||
</interpolation>
|
||||
<center>
|
||||
<x-m>4.84</x-m>
|
||||
<y-m>0.0</y-m>
|
||||
<z-m>-0.17</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>ElevatorTrimTab</object-name>
|
||||
<property>controls/flight/elevator-trim</property>
|
||||
<factor>25</factor>
|
||||
<center>
|
||||
<x-m>5.06</x-m>
|
||||
<y-m>1.12</y-m>
|
||||
<z-m>-0.18</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.17</x>
|
||||
<y>-0.82</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>Rudder</object-name>
|
||||
<object-name>RearNavLightOn</object-name>
|
||||
<object-name>RearNavLightOff</object-name>
|
||||
<property>surface-positions/rudder-pos-norm</property>
|
||||
<factor>17.5</factor>
|
||||
<center>
|
||||
<x-m>4.84</x-m>
|
||||
<y-m>0.0</y-m>
|
||||
<z-m>-.16</z-m>
|
||||
</center>
|
||||
<axis>
|
||||
<x>0.25</x>
|
||||
<y>0.0</y>
|
||||
<z>1.0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,48 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
label-bcn
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
This is an instrument configuration file for the open-source flight
|
||||
simulator FlightGear (www.flightgear.org). The file is an XML-encoded
|
||||
FlightGear property list defining the instrument's layers and actions.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labelbcn</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.47</x1>
|
||||
<y1>0.39</y1>
|
||||
<x2>0.65</x2>
|
||||
<y2>0.52</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,42 +0,0 @@
|
|||
<!--
|
||||
label-lng
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labellng</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.65</x1>
|
||||
<y1>0.49</y1>
|
||||
<x2>0.82</x2>
|
||||
<y2>0.62</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,43 +0,0 @@
|
|||
<!--
|
||||
|
||||
label-nav
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labelnav</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.47</x1>
|
||||
<y1>0.50</y1>
|
||||
<x2>0.65</x2>
|
||||
<y2>0.63</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,42 +0,0 @@
|
|||
<!--
|
||||
label-pto
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labelbcn</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.47</x1>
|
||||
<y1>0.29</y1>
|
||||
<x2>0.65</x2>
|
||||
<y2>0.42</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,42 +0,0 @@
|
|||
<!--
|
||||
label-sto
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labelbcn</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.65</x1>
|
||||
<y1>0.39</y1>
|
||||
<x2>0.82</x2>
|
||||
<y2>0.52</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,42 +0,0 @@
|
|||
<!--
|
||||
label-tax
|
||||
|
||||
Started summer 2000 by David Megginson, david@megginson.com.
|
||||
|
||||
Each instrument is composed of layers stacked on top of each other.
|
||||
A layer may be a texture (with transparent parts to show the layers
|
||||
underneath), text, or a special layer that switches between two
|
||||
others (say, to turn an indicator light on or off). Each layer can
|
||||
move independently in proportion to a property value, and text
|
||||
can be generated from property values as well: all of the layer's
|
||||
movements are defined as transformations.
|
||||
|
||||
Actions are hotspots on the instrument that will respond to a mouse
|
||||
click. Actions always modify the values of properties, either by
|
||||
adjusting them, toggling them, or swaping them with other
|
||||
properties' values.
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<name>labelbcn</name>
|
||||
|
||||
<w-base>14</w-base>
|
||||
<h-base>12</h-base>
|
||||
|
||||
<layers>
|
||||
|
||||
<layer>
|
||||
<name>face</name>
|
||||
<texture>
|
||||
<path>Aircraft/Instruments/Textures/flaps.rgb</path>
|
||||
<x1>0.65</x1>
|
||||
<y1>0.29</y1>
|
||||
<x2>0.82</x2>
|
||||
<y2>0.42</y2>
|
||||
</texture>
|
||||
</layer>
|
||||
|
||||
</layers>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,274 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!-- KAP 140 Autopilot Configuration -->
|
||||
|
||||
<!-- Each component is evaluated in the order specified. You can make up -->
|
||||
<!-- property names to pass the result of one component on to a subsequent -->
|
||||
<!-- component. -->
|
||||
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Roll Axis Modes -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<!-- Nav hold (NAV) Mode-->
|
||||
|
||||
<pid-controller>
|
||||
<name>Nav hold (NAV) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/nav-hold</prop>
|
||||
<value>nav</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/instrumentation/nav/heading-needle-deflection</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0.0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-intercept-angle</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>2.0</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-45.0</u_min> <!-- minimum output clamp -->
|
||||
<u_max>45.0</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- Approach hold (APR) Mode-->
|
||||
<pid-controller>
|
||||
<name>Approach hold (APR) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/apr-hold</prop>
|
||||
<value>apr</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/instrumentation/nav/heading-needle-deflection</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0.0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-intercept-angle</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>2.0</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.001</Td> <!-- derivator time -->
|
||||
<u_min>-45.0</u_min> <!-- minimum output clamp -->
|
||||
<u_max>45.0</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- Backcourse hold (REV) Mode-->
|
||||
<pid-controller>
|
||||
<name>Backcourse hold (REV) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/rev-hold</prop>
|
||||
<value>rev</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/instrumentation/nav/heading-needle-deflection</prop>
|
||||
<scale>-1.0</scale>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0.0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-intercept-angle</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>2.0</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-45.0</u_min> <!-- minimum output clamp -->
|
||||
<u_max>45.0</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- Heading Select (HDG) Mode -->
|
||||
|
||||
<pid-controller>
|
||||
<name>Heading Select (HDG) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/hdg-hold</prop>
|
||||
<value>hdg</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/autopilot/internal/heading-bug-error-deg</prop> -->
|
||||
<!-- <prop>/instrumentation/gps/true-bug-error-deg</prop> -->
|
||||
</input>
|
||||
<reference>
|
||||
<prop>/autopilot/KAP140/settings/target-intercept-angle</prop>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-turn-rate</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>-0.05</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-1.0</u_min> <!-- minimum output clamp -->
|
||||
<u_max>1.0</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- Wing leveler (ROL) Mode -->
|
||||
|
||||
<pid-controller>
|
||||
<name>Wing Leveler (ROL) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/roll-axis</prop>
|
||||
<value>trn</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/instrumentation/turn-indicator/indicated-turn-rate</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<prop>/autopilot/KAP140/settings/target-turn-rate</prop>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/controls/flight/aileron</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.15</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-0.25</u_min> <!-- minimum output clamp -->
|
||||
<u_max>0.25</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- =============================================================== -->
|
||||
<!-- Pitch Axis Modes -->
|
||||
<!-- =============================================================== -->
|
||||
|
||||
<!-- Altitude Hold (ALT) Mode -->
|
||||
<pid-controller>
|
||||
<name>Altitude Hold (ALT) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/alt-hold</prop>
|
||||
<value>alt</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/systems/static[0]/pressure-inhg[0]</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<prop>/autopilot/KAP140/settings/target-alt-pressure</prop>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-pressure-rate</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.125</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>12.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-0.007</u_min> <!-- minimum output clamp -->
|
||||
<u_max>0.007</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<!-- Glideslope Hold (GS) Mode -->
|
||||
<pid-controller>
|
||||
<name>Glideslope Hold (GS) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/gs-hold</prop>
|
||||
<value>gs</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/instrumentation/nav/gs-needle-deflection</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<value>0.0</value>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/autopilot/KAP140/settings/target-pressure-rate</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>0.025</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>15.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-0.001</u_min> <!-- minimum output clamp -->
|
||||
<u_max>0.017</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
<filter>
|
||||
<name>pressure-rate-filter</name>
|
||||
<debug>false</debug>
|
||||
<type>double-exponential</type>
|
||||
<input>/autopilot/internal/pressure-rate</input>
|
||||
<output>/autopilot/internal/filtered-pressure-rate</output>
|
||||
<filter-time>0.1</filter-time>
|
||||
</filter>
|
||||
|
||||
<!-- Vertical Speed (VS) Mode -->
|
||||
<pid-controller>
|
||||
<name>Vertical Speed (VS) Mode</name>
|
||||
<debug>false</debug>
|
||||
<enable>
|
||||
<prop>/autopilot/KAP140/locks/pitch-axis</prop>
|
||||
<value>vs</value>
|
||||
</enable>
|
||||
<input>
|
||||
<prop>/autopilot/internal/filtered-pressure-rate</prop>
|
||||
</input>
|
||||
<reference>
|
||||
<prop>/autopilot/KAP140/settings/target-pressure-rate</prop>
|
||||
</reference>
|
||||
<output>
|
||||
<prop>/controls/flight/elevator</prop>
|
||||
</output>
|
||||
<config>
|
||||
<Kp>5.0</Kp> <!-- proportional gain -->
|
||||
<beta>1.0</beta> <!-- input value weighing factor -->
|
||||
<alpha>0.1</alpha> <!-- low pass filter weighing factor -->
|
||||
<gamma>0.0</gamma> <!-- input value weighing factor for -->
|
||||
<!-- unfiltered derivative error -->
|
||||
<Ti>4.0</Ti> <!-- integrator time -->
|
||||
<Td>0.0</Td> <!-- derivator time -->
|
||||
<u_min>-0.5</u_min> <!-- minimum output clamp -->
|
||||
<u_max>0.5</u_max> <!-- maximum output clamp -->
|
||||
</config>
|
||||
</pid-controller>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,7 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList include="../c172p/c172p-set.xml">
|
||||
<sim>
|
||||
<description>Alias for c172p-3d.</description>
|
||||
</sim>
|
||||
</PropertyList>
|
||||
|
|
@ -1,34 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
LaRCsim Cessna 172 with 2D panel.
|
||||
used by FGFS to represent the C172. Components include the flight data
|
||||
model, instrument panel, and external 3D model.
|
||||
3D models can be downloaded from http://home.t-online.de/home/Wolfram.Kuss/
|
||||
|
||||
October 23 2001 John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="../c172p/c172p-base.xml">
|
||||
|
||||
<sim>
|
||||
|
||||
<description>Cessna 172 (LaRCsim, 2D panel).</description>
|
||||
|
||||
<flight-model>larcsim</flight-model>
|
||||
<aero>c172</aero>
|
||||
|
||||
<panel>
|
||||
<path>Aircraft/c172/Panels/c172-vfr-panel.xml</path>
|
||||
<visibility>true</visibility>
|
||||
</panel>
|
||||
<panel_2>
|
||||
<path>Aircraft/c172/Panels/c172-trans-mini-panel.xml</path>
|
||||
</panel_2>
|
||||
|
||||
</sim>
|
||||
|
||||
</PropertyList>
|
||||
|
||||
|
||||
|
|
@ -1,7 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList include="../c172p/c172p-set.xml">
|
||||
<sim>
|
||||
<description>Alias for c172p.</description>
|
||||
</sim>
|
||||
</PropertyList>
|
||||
|
|
@ -1,37 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
JSBSim Cessna 172P with 2D panel.
|
||||
|
||||
Started October 23 2001 by John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="c172p-set.xml">
|
||||
|
||||
<sim>
|
||||
|
||||
<description>Cessna 172P Skyhawk (1981 model), 2D panel</description>
|
||||
|
||||
<!-- Use a 2D instrument panel -->
|
||||
|
||||
<panel>
|
||||
<path>Aircraft/c172/Panels/c172-vfr-panel.xml</path>
|
||||
<visibility archive="y">true</visibility>
|
||||
</panel>
|
||||
<panel_2>
|
||||
<path>Aircraft/c172/Panels/c172-trans-mini-panel.xml</path>
|
||||
</panel_2>
|
||||
|
||||
<!-- Look down a bit over the top of the panel -->
|
||||
|
||||
<view>
|
||||
<internal archive="y">false</internal>
|
||||
<config>
|
||||
<pitch-offset-deg>-8</pitch-offset-deg>
|
||||
</config>
|
||||
</view>
|
||||
|
||||
</sim>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,116 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
JSBSim Cessna 172P with 3D cockpit.
|
||||
|
||||
Started October 23 2001 by John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<sim>
|
||||
|
||||
<description>Cessna 172P Skyhawk (1981 model)</description>
|
||||
<author>David Megginson</author>
|
||||
<status>production</status>
|
||||
|
||||
<flight-model archive="y">jsb</flight-model>
|
||||
<aero archive="y">c172p</aero>
|
||||
|
||||
<model>
|
||||
<path archive="y">Aircraft/c172p/Models/c172p.xml</path>
|
||||
</model>
|
||||
|
||||
<!-- hide the 2D panel -->
|
||||
|
||||
<panel>
|
||||
<visibility archive="y">false</visibility>
|
||||
</panel>
|
||||
|
||||
<!-- position the pilot viewpoint and angle -->
|
||||
|
||||
<view>
|
||||
<internal archive="y">true</internal>
|
||||
<config>
|
||||
<x-offset-m archive="y">-0.21</x-offset-m>
|
||||
<y-offset-m archive="y">0.30</y-offset-m>
|
||||
<z-offset-m archive="y">0.36</z-offset-m>
|
||||
<pitch-offset-deg>-12</pitch-offset-deg>
|
||||
</config>
|
||||
</view>
|
||||
|
||||
<systems>
|
||||
<autopilot>
|
||||
<path>Aircraft/c172p/Systems/KAP140.xml</path>
|
||||
</autopilot>
|
||||
<electrical>
|
||||
<path>Aircraft/c172/c172-electrical.xml</path>
|
||||
</electrical>
|
||||
</systems>
|
||||
|
||||
<sound>
|
||||
<path archive="y">Aircraft/c172/c172-sound.xml</path>
|
||||
</sound>
|
||||
|
||||
</sim>
|
||||
|
||||
<!-- trim for level cruise -->
|
||||
|
||||
<controls>
|
||||
<flight>
|
||||
<aileron-trim>0.027</aileron-trim>
|
||||
<rudder-trim>0.0</rudder-trim>
|
||||
</flight>
|
||||
<engines>
|
||||
<engine n="0">
|
||||
<magnetos>3</magnetos>
|
||||
</engine>
|
||||
</engines>
|
||||
</controls>
|
||||
|
||||
<autopilot>
|
||||
<config>
|
||||
<min-climb-speed-kt type="float">70.0</min-climb-speed-kt>
|
||||
<best-climb-speed-kt type="float">75.0</best-climb-speed-kt>
|
||||
<target-climb-rate-fpm type="float">500.0</target-climb-rate-fpm>
|
||||
<target-descent-rate-fpm type="float">1000.0</target-descent-rate-fpm>
|
||||
<elevator-adj-factor type="float">4000.0</elevator-adj-factor>
|
||||
<integral-contribution type="float">0.01</integral-contribution>
|
||||
<zero-pitch-throttle type="float">0.45</zero-pitch-throttle>
|
||||
<zero-pitch-trim-full-throttle type="float">0.14</zero-pitch-trim-full-throttle>
|
||||
</config>
|
||||
</autopilot>
|
||||
|
||||
<consumables>
|
||||
<fuel>
|
||||
<tank n="0">
|
||||
<level-gal_us>20</level-gal_us>
|
||||
</tank>
|
||||
<tank n="1">
|
||||
<level-gal_us>20</level-gal_us>
|
||||
</tank>
|
||||
</fuel>
|
||||
</consumables>
|
||||
|
||||
<instrumentation>
|
||||
<attitude-indicator>
|
||||
<config>
|
||||
<tumble-flag archive="y" type="bool">true</tumble-flag>
|
||||
</config>
|
||||
</attitude-indicator>
|
||||
</instrumentation>
|
||||
|
||||
<engines>
|
||||
<engine>
|
||||
<rpm type="double">700</rpm>
|
||||
</engine>
|
||||
</engines>
|
||||
|
||||
<nasal>
|
||||
<kap140>
|
||||
<file>Aircraft/c172p/kap140.nas</file>
|
||||
</kap140>
|
||||
</nasal>
|
||||
|
||||
</PropertyList>
|
||||
|
|
@ -1,677 +0,0 @@
|
|||
<FDM_CONFIG NAME="c172" VERSION="1.65">
|
||||
<!--
|
||||
File: c172p.xml
|
||||
Author: David Megginson (based on c172r.xml by Tony Peden)
|
||||
CVS Version: $Id$
|
||||
|
||||
Function: Models a 1981 Cessna 172P.
|
||||
|
||||
Sources:
|
||||
Tony Peden, c172r.xml, JSBSim (http://jsbsim.sourceforge.net/).
|
||||
Jan Roskam, Airplane Flight Dynamics and Automatic Flight
|
||||
Controls. Part I. DARcorporation, 1995.
|
||||
|
||||
Notes:
|
||||
|
||||
Roskam's data is for a 182, not a 172, but it should be close
|
||||
enough. He gives linear coefficients for three states:
|
||||
|
||||
1. Climb (5.4 deg alpha).
|
||||
2. Cruise (0 deg alpha).
|
||||
3. Approach (4 deg alpha, and presumably, full flaps).
|
||||
|
||||
I have extrapolated small tables from this data to account for the
|
||||
effects of flaps and alpha, especially in the lateral coefficients.
|
||||
-->
|
||||
|
||||
<METRICS>
|
||||
<!--
|
||||
// Wing area (ft^2)
|
||||
// Wing span (ft)
|
||||
// Wing avg. chord (ft)
|
||||
// H. Tail Area (ft^2)
|
||||
// Wing MAC to H.Tail MAC (ft)
|
||||
// V. Tail Area (ft^2)
|
||||
// Wing MAC to V.Tail MAC (ft)
|
||||
// Ixx
|
||||
// Iyy
|
||||
// Izz
|
||||
// Ixz
|
||||
// Empty weight
|
||||
// Center of gravity location, empty weight, in aircraft's own structural coord
|
||||
// system. X, Y, Z, in inches
|
||||
// Pilot's eyepoint location, in aircraft's own coord system, FROM cg.
|
||||
// X, Y, Z, in inches
|
||||
AC_AERORP 43.2 0.0 59.4
|
||||
-->
|
||||
|
||||
AC_WINGAREA 174 <!-- square feet -->
|
||||
AC_WINGSPAN 35.8 <!-- ft -->
|
||||
AC_CHORD 4.9 <!-- ft -->
|
||||
AC_HTAILAREA 21.9 <!-- square feet -->
|
||||
AC_HTAILARM 15.7 <!-- ft -->
|
||||
AC_VTAILAREA 16.5 <!-- square feet -->
|
||||
AC_LV 15.7 <!-- ft -->
|
||||
AC_IXX 948
|
||||
AC_IYY 1346
|
||||
AC_IZZ 1967
|
||||
AC_IXZ 0
|
||||
AC_EMPTYWT 1500
|
||||
AC_AERORP 43.2 0.0 59.4
|
||||
AC_CGLOC 41.0 0.0 36.5
|
||||
<!-- Pilot -->
|
||||
AC_POINTMASS 180.0 36.0 -14.0 24.0
|
||||
<!-- Co-pilot -->
|
||||
<!-- AC_POINTMASS 180.0 36.0 14.0 24.0 -->
|
||||
AC_EYEPTLOC 37.0 0.0 48.0
|
||||
AC_VRP 42.6 0.0 38.5
|
||||
</METRICS>
|
||||
|
||||
<UNDERCARRIAGE>
|
||||
|
||||
<!--
|
||||
The gear parameters that can be specified are as follows, IN ORDER OF APPEARANCE:
|
||||
|
||||
AC_GEAR
|
||||
<name> name of gear entry - no spaces allowed
|
||||
<X> <Y> <Z> Gear location in aircraft body coords in inches
|
||||
<spring constant> spring constant in lbs/ft
|
||||
<damping coefficient> damping coefficient in lbs/ft/sec
|
||||
<dynamic friction coefficient> Self-explanatory: sliding friction coefficient
|
||||
<static friction coefficient> Self-explanatory: "onset" friction coefficient
|
||||
<rolling friction coefficient> Self-explanatory: rolling friction coefficient
|
||||
<steerability attribute> One of <STEERABLE | FIXED | CASTERED>
|
||||
<brake group membership> One of <LEFT | CENTER | RIGHT | NOSE | TAIL | NONE>
|
||||
<max steer angle> Maximum steerable angle in degrees
|
||||
<retraction attribute> <RETRACT | FIXED>
|
||||
-->
|
||||
|
||||
AC_GEAR NOSE -6.8 0.0 -20.0 1800 600 0.5 0.8 0.02 STEERABLE NONE 10 FIXED
|
||||
AC_GEAR LEFT_MAIN 58.2 -43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED LEFT 0 FIXED
|
||||
AC_GEAR RIGHT_MAIN 58.2 43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED RIGHT 0 FIXED
|
||||
AC_GEAR TAIL_SKID 188.0 0.0 8.0 20000 1000 0.2 0.2 0.2 FIXED NONE 0 FIXED
|
||||
AC_GEAR LEFT_TIP 43.2 -214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED
|
||||
AC_GEAR RIGHT_TIP 43.2 214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED
|
||||
|
||||
</UNDERCARRIAGE>
|
||||
|
||||
<PROPULSION>
|
||||
|
||||
<!--
|
||||
TANKS SECTION
|
||||
|
||||
Tank locations and characteristics, empty weight, in aircraft's own coord system:
|
||||
X, Y, Z, in inches
|
||||
effective radius of tank, in inches (for fuel slosh, if/when modeled)
|
||||
capacity in pounds
|
||||
Current contents, in pounds
|
||||
|
||||
ENGINE[S] SECTION
|
||||
|
||||
Engine[s] is|are specified by giving engine name (which corresponds to an engine
|
||||
definition file in the "engines" directory) followed by x, y, z placement and
|
||||
pitch and yaw orientation. Coordinates are given in inches in the structural
|
||||
coordinate frame. Angles for pitch and yaw are specified in radians.
|
||||
|
||||
AC_ENGINE name x y z pitch yaw
|
||||
|
||||
THRUSTER[S] SECTION
|
||||
|
||||
AC_THRUSTER name x y z pitch yaw
|
||||
-->
|
||||
|
||||
<AC_ENGINE FILE="eng_io320">
|
||||
XLOC -19.7
|
||||
YLOC 0.0
|
||||
ZLOC 26.6
|
||||
PITCH 0.0
|
||||
YAW 0.0
|
||||
FEED 0
|
||||
FEED 1
|
||||
<AC_THRUSTER FILE="prop_75in2f">
|
||||
XLOC -37.7
|
||||
YLOC 0.0
|
||||
ZLOC 26.6
|
||||
PITCH 0.0
|
||||
YAW 0
|
||||
P_FACTOR 10.0
|
||||
SENSE 1.0
|
||||
</AC_THRUSTER>
|
||||
</AC_ENGINE>
|
||||
|
||||
<AC_TANK TYPE="FUEL" NUMBER="0">
|
||||
XLOC 56.0
|
||||
YLOC -112.0
|
||||
ZLOC 59.4
|
||||
RADIUS 29.4
|
||||
CAPACITY 185.0
|
||||
CONTENTS 100.0
|
||||
</AC_TANK>
|
||||
|
||||
<AC_TANK TYPE="FUEL" NUMBER="1">
|
||||
XLOC 56.0
|
||||
YLOC 112.0
|
||||
ZLOC 59.4
|
||||
RADIUS 29.4
|
||||
CAPACITY 185.0
|
||||
CONTENTS 100.0
|
||||
</AC_TANK>
|
||||
|
||||
</PROPULSION>
|
||||
|
||||
|
||||
<FLIGHT_CONTROL NAME="c172">
|
||||
<COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
|
||||
INPUT fcs/elevator-cmd-norm
|
||||
INPUT fcs/pitch-trim-cmd-norm
|
||||
CLIPTO -1 1
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
|
||||
INPUT fcs/pitch-trim-sum
|
||||
MIN -28
|
||||
MAX 23
|
||||
OUTPUT fcs/elevator-pos-rad
|
||||
GAIN 0.01745
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
|
||||
INPUT fcs/aileron-cmd-norm
|
||||
INPUT fcs/roll-trim-cmd-norm
|
||||
CLIPTO -1 1
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
|
||||
INPUT fcs/roll-trim-sum
|
||||
MIN -20
|
||||
MAX 15
|
||||
GAIN 0.01745
|
||||
OUTPUT fcs/left-aileron-pos-rad
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
|
||||
INPUT fcs/roll-trim-sum
|
||||
MIN -20
|
||||
MAX 15
|
||||
GAIN -0.01745
|
||||
OUTPUT fcs/right-aileron-pos-rad
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Yaw Trim Sum" TYPE="SUMMER">
|
||||
INPUT fcs/rudder-cmd-norm
|
||||
INPUT fcs/yaw-trim-cmd-norm
|
||||
CLIPTO -1 1
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
|
||||
INPUT fcs/yaw-trim-sum
|
||||
MIN -16
|
||||
MAX 16
|
||||
GAIN 0.01745
|
||||
OUTPUT fcs/rudder-pos-rad
|
||||
</COMPONENT>
|
||||
<COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
|
||||
INPUT fcs/flap-cmd-norm
|
||||
DETENTS 4
|
||||
0 0
|
||||
10 2
|
||||
20 1
|
||||
30 1
|
||||
OUTPUT fcs/flap-pos-deg
|
||||
</COMPONENT>
|
||||
</FLIGHT_CONTROL>
|
||||
|
||||
<AERODYNAMICS>
|
||||
|
||||
AC_ALPHALIMITS -0.087 0.28
|
||||
AC_HYSTLIMITS 0.09 0.36
|
||||
|
||||
<AXIS NAME="LIFT">
|
||||
|
||||
<GROUP NAME="CLb">
|
||||
Basic_lift
|
||||
|
||||
<!-- Peden -->
|
||||
<FACTOR NAME="kCLge" TYPE="VECTOR">
|
||||
Change_in_lift_due_to_ground_effect
|
||||
13
|
||||
aero/h_b-mac-ft
|
||||
none
|
||||
0.0 1.203
|
||||
0.1 1.127
|
||||
0.15 1.090
|
||||
0.2 1.073
|
||||
0.3 1.046
|
||||
0.4 1.055
|
||||
0.5 1.019
|
||||
0.6 1.013
|
||||
0.7 1.008
|
||||
0.8 1.006
|
||||
0.9 1.003
|
||||
1.0 1.002
|
||||
1.1 1.0
|
||||
</FACTOR>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="CLwbh" TYPE="TABLE">
|
||||
Lift_due_to_alpha
|
||||
17
|
||||
2
|
||||
aero/alpha-rad
|
||||
aero/stall-hyst-norm
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0 1
|
||||
-0.09 -0.22 -0.22
|
||||
0 0.25 0.25
|
||||
0.09 0.73 0.73
|
||||
0.1 0.83 0.78
|
||||
0.12 0.92 0.79
|
||||
0.14 1.02 0.81
|
||||
0.16 1.08 0.82
|
||||
0.17 1.13 0.83
|
||||
0.19 1.19 0.85
|
||||
0.21 1.25 0.86
|
||||
0.24 1.35 0.88
|
||||
0.26 1.44 0.9
|
||||
0.28 1.47 0.92
|
||||
0.3 1.43 0.95
|
||||
0.32 1.38 0.99
|
||||
0.34 1.3 1.05
|
||||
0.36 1.15 1.15
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="CLDf" TYPE="VECTOR">
|
||||
Delta_lift_due_to_flap_deflection
|
||||
4
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0 0
|
||||
10 0.20
|
||||
20 0.30
|
||||
30 0.35
|
||||
</COEFFICIENT>
|
||||
|
||||
</GROUP>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="CLDe" TYPE="VALUE">
|
||||
Lift_due_to_Elevator_Deflection
|
||||
aero/qbar-psf | metrics/Sw-sqft | fcs/elevator-pos-rad
|
||||
0.43
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="CLadot" TYPE="VALUE">
|
||||
Lift_due_to_alpha_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | aero/alphadot-rad_sec | aero/ci2vel
|
||||
1.7
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="CLq" TYPE="VALUE">
|
||||
Lift_due_to_pitch_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | velocities/q-aero-rad_sec | aero/ci2vel
|
||||
3.9
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
<AXIS NAME="DRAG">
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="CDo" TYPE="VALUE">
|
||||
Drag_at_zero_lift
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0.0270
|
||||
</COEFFICIENT>
|
||||
|
||||
<GROUP NAME="CDb">
|
||||
Basic_drag
|
||||
|
||||
<!-- Peden -->
|
||||
<FACTOR NAME="kCDge" TYPE="VECTOR">
|
||||
Change_in_drag_due_to_ground_effect
|
||||
13
|
||||
aero/h_b-mac-ft
|
||||
none
|
||||
0.0 0.048
|
||||
0.1 0.515
|
||||
0.15 0.629
|
||||
0.2 0.709
|
||||
0.3 0.815
|
||||
0.4 0.882
|
||||
0.5 0.928
|
||||
0.6 0.962
|
||||
0.7 0.988
|
||||
0.8 1.0
|
||||
0.9 1.0
|
||||
1.0 1.0
|
||||
1.1 1.0
|
||||
</FACTOR>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="CDDf" TYPE="VECTOR">
|
||||
Delta_drag_due_to_flap_deflection
|
||||
4
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0 0
|
||||
10 0.007
|
||||
20 0.012
|
||||
30 0.018
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="CDwbh" TYPE="TABLE">
|
||||
Drag_due_to_alpha
|
||||
26
|
||||
4
|
||||
aero/alpha-rad
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0 10 20 30
|
||||
-0.0872664 0.00407143 3.8165e-05 0.000512444 0.00137231
|
||||
-0.0698132 0.0013424 0.000440634 0.00248067 0.00412341
|
||||
-0.0523599 8.96747e-05 0.00231942 0.0059252 0.00835082
|
||||
-0.0349066 0.000313268 0.00567451 0.0108461 0.0140545
|
||||
-0.0174533 0.00201318 0.0105059 0.0172432 0.0212346
|
||||
0 0.0051894 0.0168137 0.0251167 0.0298909
|
||||
0.0174533 0.00993967 0.0247521 0.0346492 0.0402205
|
||||
0.0349066 0.0162201 0.0342207 0.0457119 0.0520802
|
||||
0.0523599 0.0240308 0.0452195 0.0583047 0.0654701
|
||||
0.0698132 0.0333717 0.0577485 0.0724278 0.0803902
|
||||
0.0872664 0.0442427 0.0718077 0.088081 0.0968405
|
||||
0.10472 0.056644 0.0873971 0.105265 0.114821
|
||||
0.122173 0.0705754 0.104517 0.123978 0.134332
|
||||
0.139626 0.086037 0.123166 0.144222 0.155373
|
||||
0.15708 0.096239 0.135317 0.157346 0.168984
|
||||
0.174533 0.106859 0.147857 0.170848 0.182966
|
||||
0.191986 0.118034 0.160954 0.184905 0.197503
|
||||
0.209439 0.129765 0.174606 0.199517 0.212596
|
||||
0.226893 0.142366 0.189176 0.215072 0.228643
|
||||
0.244346 0.156452 0.205363 0.23231 0.246406
|
||||
0.261799 0.172732 0.223956 0.252059 0.266733
|
||||
0.279253 0.178209 0.230187 0.258667 0.273529
|
||||
0.296706 0.171598 0.222665 0.25069 0.265325
|
||||
0.314159 0.161786 0.211468 0.2388 0.253089
|
||||
0.331613 0.147493 0.19508 0.221364 0.235129
|
||||
0.349066 0.109678 0.151171 0.174408 0.186649
|
||||
</COEFFICIENT>
|
||||
|
||||
</GROUP>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="CDDe" TYPE="VALUE">
|
||||
Drag_due_to_Elevator_Deflection
|
||||
aero/qbar-psf | metrics/Sw-sqft | fcs/mag-elevator-pos-rad
|
||||
0
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="CDbeta" TYPE="VALUE">
|
||||
Drag_due_to_sideslip
|
||||
aero/qbar-psf | metrics/Sw-sqft | aero/mag-beta-rad
|
||||
0.17
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
<AXIS NAME="SIDE">
|
||||
|
||||
<!-- based on Roskam p.482, clamped to +/-20deg beta -->
|
||||
<COEFFICIENT NAME="CYb" TYPE="TABLE">
|
||||
Side_force_due_to_beta
|
||||
3
|
||||
2
|
||||
aero/beta-rad
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft
|
||||
0 30
|
||||
-0.349 0.137 0.106
|
||||
0 0 0
|
||||
0.349 -0.137 -0.106
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="CYda" TYPE="VALUE">
|
||||
Side_force_due_to_aileron
|
||||
aero/qbar-psf | metrics/Sw-sqft | fcs/left-aileron-pos-rad
|
||||
0
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="CYdr" TYPE="VALUE">
|
||||
Side_force_due_to_rudder
|
||||
aero/qbar-psf | metrics/Sw-sqft | fcs/rudder-pos-rad
|
||||
0.187
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- based on Roskam p.482 -->
|
||||
<COEFFICIENT NAME="CYp" TYPE="TABLE">
|
||||
Side_force_due_to_roll_rate
|
||||
2
|
||||
2
|
||||
aero/alpha-rad
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/p-aero-rad_sec
|
||||
0 30
|
||||
0.000 -0.075 -0.161
|
||||
0.094 -0.145 -0.231
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- based on Roskam p.482 -->
|
||||
<COEFFICIENT NAME="CYr" TYPE="TABLE">
|
||||
Side_force_due_to_yaw_rate
|
||||
2
|
||||
2
|
||||
aero/alpha-rad
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/r-aero-rad_sec
|
||||
0 30
|
||||
0.000 0.214 0.162
|
||||
0.094 0.267 0.215
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
<AXIS NAME="ROLL">
|
||||
|
||||
<!-- based on Roskam p.482, clamped to +/-20deg beta -->
|
||||
<COEFFICIENT NAME="Clb" TYPE="VECTOR">
|
||||
Roll_moment_due_to_beta
|
||||
3
|
||||
aero/beta-rad
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft
|
||||
-0.349 0.0322
|
||||
0 0
|
||||
0.349 -0.0322
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="Clp" TYPE="VALUE">
|
||||
Roll_moment_due_to_roll_rate_(roll_damping)
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec
|
||||
-0.484
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- based on Roskam p.482 -->
|
||||
<COEFFICIENT NAME="Clr" TYPE="TABLE">
|
||||
Roll_moment_due_to_yaw_rate
|
||||
2
|
||||
2
|
||||
aero/alpha-rad
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec
|
||||
0 30
|
||||
0.000 0.0798 0.1246
|
||||
0.094 0.1869 0.2317
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="ClDa" TYPE="VALUE">
|
||||
Roll_moment_due_to_aileron
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad
|
||||
0.229
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="Cldr" TYPE="VALUE">
|
||||
Roll_moment_due_to_rudder
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad
|
||||
0.0147
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
<AXIS NAME="PITCH">
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="Cmo" TYPE="VALUE">
|
||||
Pitching_moment_at_zero_alpha
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft
|
||||
0.1
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
|
||||
Pitch_moment_due_to_alpha
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/alpha-rad
|
||||
-1.8
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="Cmq" TYPE="VALUE">
|
||||
Pitch_moment_due_to_pitch_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | velocities/q-aero-rad_sec
|
||||
-12.4
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- based on Roskam p.481 -->
|
||||
<COEFFICIENT NAME="Cmadot" TYPE="VALUE">
|
||||
Pitch_moment_due_to_alpha_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | aero/alphadot-rad_sec
|
||||
-7.27
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.481 -->
|
||||
<COEFFICIENT NAME="Cmde" TYPE="VALUE">
|
||||
Pitch_moment_due_to_elevator_deflection
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | fcs/elevator-pos-rad
|
||||
-1.122
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="Cmdf" TYPE="VECTOR">
|
||||
Delta_pitching_moment_due_to_flap_deflection
|
||||
4
|
||||
fcs/flap-pos-deg
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft
|
||||
0 0
|
||||
10 -0.0654
|
||||
20 -0.0981
|
||||
30 -0.1140
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
<AXIS NAME="YAW">
|
||||
|
||||
<!-- based on Roskam p.482, clamped to +/-20deg beta -->
|
||||
<COEFFICIENT NAME="Cnb" TYPE="VECTOR">
|
||||
Yaw_moment_due_to_beta
|
||||
3
|
||||
aero/beta-rad
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft
|
||||
-0.349 -0.0205
|
||||
0 0
|
||||
0.349 0.0205
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="Cnp" TYPE="VALUE">
|
||||
Yaw_moment_due_to_roll_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec
|
||||
-0.0278
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Roskam p.482 -->
|
||||
<COEFFICIENT NAME="Cnr" TYPE="VALUE">
|
||||
Yaw_moment_due_to_yaw_rate
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec
|
||||
-0.0937
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="Cnda" TYPE="VALUE">
|
||||
Yaw_moment_due_to_aileron
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad
|
||||
-0.0053
|
||||
</COEFFICIENT>
|
||||
|
||||
<!-- Peden -->
|
||||
<COEFFICIENT NAME="Cndr" TYPE="VALUE">
|
||||
Yaw_moment_due_to_rudder
|
||||
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad
|
||||
-0.043
|
||||
</COEFFICIENT>
|
||||
|
||||
</AXIS>
|
||||
|
||||
</AERODYNAMICS>
|
||||
|
||||
<!--
|
||||
OUTPUT section definition
|
||||
|
||||
The following specifies the way that JSBSim writes out data.
|
||||
|
||||
NAME is the filename you want the output to go to
|
||||
|
||||
TYPE can be:
|
||||
CSV Comma separated data. If a filename is supplied then the data
|
||||
goes to that file. If COUT or cout is specified, the data goes
|
||||
to stdout. If the filename is a null filename the data goes to
|
||||
stdout, as well.
|
||||
SOCKET Will eventually send data to a socket output, where NAME
|
||||
would then be the IP address of the machine the data should be
|
||||
sent to. DON'T USE THIS YET!
|
||||
TABULAR Columnar data. NOT IMPLEMENTED YET!
|
||||
TERMINAL Output to terminal. NOT IMPLEMENTED YET!
|
||||
NONE Specifies to do nothing. THis setting makes it easy to turn on and
|
||||
off the data output without having to mess with anything else.
|
||||
|
||||
The arguments that can be supplied, currently, are
|
||||
|
||||
RATE_IN_HZ An integer rate in times-per-second that the data is output. This
|
||||
value may not be *exactly* what you want, due to the dependence
|
||||
on dt, the cycle rate for the FDM.
|
||||
|
||||
The following parameters tell which subsystems of data to output:
|
||||
|
||||
SIMULATION ON|OFF
|
||||
ATMOSPHERE ON|OFF
|
||||
MASSPROPS ON|OFF
|
||||
AEROSURFACES ON|OFF
|
||||
RATES ON|OFF
|
||||
VELOCITIES ON|OFF
|
||||
FORCES ON|OFF
|
||||
MOMENTS ON|OFF
|
||||
POSITION ON|OFF
|
||||
COEFFICIENTS ON|OFF
|
||||
GROUND_REACTIONS ON|OFF
|
||||
FCS ON|OFF
|
||||
PROPULSION ON|OFF
|
||||
|
||||
NOTE that Time is always output with the data.
|
||||
-->
|
||||
<OUTPUT NAME="JSBout172.csv" TYPE="NONE">
|
||||
RATE_IN_HZ 20
|
||||
SIMULATION OFF
|
||||
ATMOSPHERE ON
|
||||
MASSPROPS ON
|
||||
AEROSURFACES ON
|
||||
RATES ON
|
||||
VELOCITIES ON
|
||||
FORCES ON
|
||||
MOMENTS ON
|
||||
POSITION ON
|
||||
COEFFICIENTS ON
|
||||
GROUND_REACTIONS ON
|
||||
FCS ON
|
||||
PROPULSION ON
|
||||
</OUTPUT>
|
||||
</FDM_CONFIG>
|
||||
Loading…
Reference in a new issue