carrier_nav.dat.gz: Add missing TACAN range entries
[fg:toms-fgdata.git] / Aircraft / PC-12 / pc12-yasim.xml
1 <?xml version="1.0" encoding="ISO-8859-1"?>
2
3 <!-- Pilatus PC12/47 - 2010 Emmanuel BARANGER
4
5      sources          : http://en.wikipedia.org/wiki/Pilatus_PC-12
6
7      wingspan         :  16.23 m ( 53 ft 3 in )
8      length           :  14.40 m ( 47 ft 3 in )
9      height           :   4.26 m ( 14 ft 0 in )
10      empty weight     :  2761 kg ( 5867 lb    )
11      engine           : Pratt & Whitney Canada PT6A-67B or -67P turboprop ( 1200 hp )
12      Maximum speed    :   280 km/h ( 152 kts )
13      Cruise speed     :   500 km/h ( 270 Kts )
14 -->
15
16 <airplane mass="5867">
17
18   <!-- Approach configuration -->
19   <approach speed="80" aoa="4" fuel="0.2">
20     <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
21     <control-setting axis="/controls/engines/engine[0]/condition" value="1.0"/>
22     <control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.3"/>
23     <control-setting axis="/controls/flight/flaps" value="1.0"/>
24     <control-setting axis="/controls/gear/gear-down" value="1"/>
25   </approach>
26
27   <!-- Cruise configuration -->
28   <cruise speed="270" alt="0" fuel="0.5">
29     <control-setting axis="/controls/flight/elevator-trim" value="0"/>
30     <control-setting axis="/controls/engines/engine[0]/throttle" value="0.8"/>
31     <control-setting axis="/controls/engines/engine[0]/condition" value="1"/>
32     <control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.9"/>
33     <control-setting axis="/controls/flight/flaps" value="0"/>
34     <control-setting axis="/controls/gear/gear-down" value="0"/>
35   </cruise>
36
37   <cockpit x="3.37507" y="0.37523" z="0.28085"/>
38
39   <fuselage ax="6.58961" ay="0" az="-0.463" bx="-5.14686" by="0" bz="-0.0321" width="1.662" taper="0.4" midpoint="0.3"/>
40
41   <wing x="1.18751" y="0.339" z="-1.07958" 
42         chord="2.158" 
43         length="7.138" 
44         taper="0.6"
45         dihedral="6"
46         sweep="-2"
47         camber="0.01">
48         <stall aoa="18" width="1" peak="1.5"/>
49         <flap0 start="0.08" end="0.75" lift="1.2" drag="1.25"/>
50         <flap1 start="0.76" end="1.00" lift="1.2" drag="1.1"/>
51
52         <control-input axis="/controls/flight/flaps" control="FLAP0"/>
53         <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
54         <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
55
56         <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
57         <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
58         <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
59
60         <control-speed control="FLAP0" transition-time="2"/>
61   </wing>
62
63   <hstab x="-6.16016" y="0" z="1.95551" 
64          chord="1.266" 
65          length="2.638" 
66          taper="0.7">
67          <stall aoa="16" width="1" peak="1.5"/>
68          <flap0 start="0" end="1" lift="1.5" drag="1"/>
69
70          <control-input axis="/controls/flight/elevator" control="FLAP0"/>
71          <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
72
73          <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
74   </hstab>
75
76   <vstab x="-4.40078" y="0" z="-0.17619" 
77          chord="2.979"
78          length="2.800"
79          taper="0.40"
80          sweep="40">
81          <stall aoa="14" width="1" peak="1.5"/>
82          <flap0 start="0.02" end="0.9" lift="1.75" drag="1.35"/>
83
84          <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
85          <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
86
87          <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
88   </vstab>3.00
89
90   <!-- Engines   source            : http://en.wikipedia.org/wiki/Pratt_%26_Whitney_Canada_PT6A
91
92                  name              : Pratt & Whitney Canada PT6
93                  type              : free turbine providing 500 to 1940 shaft horsepower (433 to 1447 kW).
94  
95        For the moment is the Beechcraft Starship configuration
96   -->
97   <propeller x="5.61035" y="0.0" z="-0.40130"
98              mass="231" 
99              moment="73.211" 
100              radius="1.35"
101              cruise-speed="270" 
102              cruise-rpm="2000"
103              cruise-power="1200" 
104              cruise-alt="19000"
105              min-rpm="150" 
106              max-rpm="2000"
107              fine-stop="0.25" 
108              coarse-stop="3.0"
109              gear-ratio="0.66">
110              <actionpt x="6.72862" y="0.0" z="-0.40130"/>
111              <turbine-engine eng-power="1200" 
112                              eng-rpm="3000" 
113                              alt="19000"
114                              flat-rating="1200"
115                              min-n2="70" 
116                              max-n2="100"
117                              bsfc="0.35"/>
118              <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE" src0="0.3" src1="1.0" dst0="0.0" dst1="1.0"/>
119              <control-input axis="/controls/engines/engine[0]/condition" control="CONDLEVER"/>
120              <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
121              <control-input axis="/controls/engines/engine[0]/propeller-pitch" control="ADVANCE" src0="0.15" src1="1.0" dst0="-0.1" dst1="1.0"/>
122              <control-input axis="/controls/engines/engine[0]/propeller-pitch" control="PROPFEATHER"  src0="0.0" src1="0.15" dst0="1.0" dst1="0.0"/>
123   </propeller>
124   
125   <!-- Noze wheel -->
126   <gear x="4.68439" y="0" z="-2.02835" 
127         compression="0.15" 
128         spring="0.8"
129         on-solid="1"
130         sfric="1"
131         dfric="1">
132         <control-input axis="/controls/flight/rudder" control="STEER" square="false"/>
133         <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
134         <control-speed control="EXTEND" transition-time="7"/>
135         <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
136   </gear>
137
138   <!-- Left wheel -->
139   <gear x="1.22521" y="-2.24719" z="-2.11304"
140         compression="0.2" 
141         spring="1.8" 
142         damp="0.03" 
143         on-solid="1" >
144         <control-input axis="/controls/gear/brake-left" control="BRAKE"/>
145         <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
146         <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
147         <control-speed control="EXTEND" transition-time="7"/>
148         <control-output control="EXTEND" prop="gear/gear[1]/position-norm"/>
149   </gear>
150
151   <!-- Right wheel -->
152   <gear x="1.22521" y="2.24719" z="-2.11304"
153         compression="0.2" 
154         spring="1.8"
155         damp="0.03" 
156         on-solid="1" >
157         <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
158         <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
159         <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
160         <control-speed control="EXTEND" transition-time="7"/>
161         <control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
162   </gear>
163
164   <tank x="1.58" y=" 2.58" z="-0.85" capacity="1500" />
165   <tank x="2.50" y=" 0.00" z="-1.00" capacity="1500" />
166   <tank x="1.58" y="-2.58" z="-0.85" capacity="1500" />
167
168  <!-- Mass distribution -->
169   <ballast x="6" y="0" z="-1.6" mass="550"/>
170  
171 </airplane>