- New instruments, some little changes
[fg:toms-fgdata.git] / Aircraft / DH-88 / dh88-yasim.xml
1 <!-- D.H. 88 Comet      2008 BARANGER Emmanuel 
2
3    Envergure    : 13.4 m        ( 44'0 ft)
4    Longueur     :  8.8 m        ( 29'0 ft)
5    Hauteur      :  3.1 m        ( 10'0 ft)
6    Moteurs      : 2 x Gypsy Six (230 cv) 
7    Poids à vide : 1330 kg       ( 2930 lb)
8    Vitesse max  : 381 km/h      ( 237 mph)
9    Alttitude    : 5790 m        ( 19000 ft)
10 -->
11
12 <airplane mass="2930">
13
14   <approach speed="70" aoa="14">
15     <control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
16     <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
17     <control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
18     <control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
19     <control-setting axis="/controls/flight/flaps" value="1.0"/>
20     <control-setting axis="/controls/gear/gear-down" value="1"/>
21   </approach>
22
23   <cruise speed="195" alt="19000">
24     <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
25     <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
26     <control-setting axis="/controls/engines/engine[0]/boost" value="1.0"/>
27     <control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
28     <control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
29     <control-setting axis="/controls/engines/engine[1]/boost" value="1.0"/>
30     <control-setting axis="/controls/flight/flaps" value="0.0"/>
31     <control-setting axis="/controls/gear/gear-down" value="0"/>
32   </cruise>
33
34   <cockpit x="-0.139" y="0" z="0.58"/>
35
36   <fuselage ax="4.397" ay="0" az="0.06" bx="-4.338" by="0" bz="0.399" width="1.049" taper="0.5" midpoint="0.25"/>
37
38   <wing x="1.312" y="0.293" z="-0.219" 
39         chord="2.343" 
40         taper=".20" 
41         length="6.319" 
42         camber="0.1"
43         sweep="2" 
44         dihedral="1.5">
45         <stall aoa="14" width="6" peak="1.5"/>
46         <flap1 start="0.550" end="0.945" lift="1.2" drag="1.2"/>
47
48         <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
49         <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
50
51         <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
52         <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
53   </wing>
54
55   <hstab x="-3.504" y="0.0" z="0.391" 
56          chord="1.320" 
57          taper="0.22" 
58          length="1.851" 
59          sweep="10" 
60          incidence="0">
61          <stall aoa="18" width="3" peak="1.5"/>
62          <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
63
64          <control-input axis="/controls/flight/elevator" control="FLAP0" effectiveness="0.3"/>
65          <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
66
67          <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
68   </hstab>
69
70   <vstab x="-3.320" y="0" z="0.248" 
71          chord="1.989" 
72          taper="0.24" 
73          length="1.262"
74          sweep="35">
75          <stall aoa="14" width="3" peak="1.5"/>
76          <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
77
78          <control-input axis="/controls/flight/rudder" control="FLAP0" effectiveness="2.0" invert="true"/>
79          <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
80
81          <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
82   </vstab>
83
84   <!-- Moteur gauche -->
85   <propeller x="2.500" y="1.469" z="-0.519"
86              mass="600" 
87              moment="35" 
88              radius="1.8"
89              cruise-power="200" 
90              cruise-speed="195"
91              cruise-rpm="2300" 
92              cruise-alt="19000">
93              <piston-engine eng-rpm="2700" 
94                             eng-power="230"
95                             displacement="1220" 
96                             compression="5"/>
97              <actionpt x="3.486" y="1.468" z="-0.387"/>
98              <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
99              <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
100              <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
101              <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
102              <control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
103   </propeller>
104
105   <!-- Moteur droit -->
106   <propeller x="2.500" y="-1.469" z="-0.519"
107              mass="600" 
108              moment="-35" 
109              radius="1.8"
110              cruise-power="200" 
111              cruise-speed="195"
112              cruise-rpm="2300" 
113              cruise-alt="19000">
114              <piston-engine eng-rpm="2700" 
115                             eng-power="230"
116                             displacement="1220" 
117                             compression="5"/>
118              <actionpt x="3.486" y="-1.468" z="-0.387"/>
119              <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
120              <control-input axis="/controls/engines/engine[1]/starter" control="STARTER"/>
121              <control-input axis="/controls/engines/engine[1]/magnetos" control="MAGNETOS"/>
122              <control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
123              <control-input axis="/controls/engines/engine[1]/boost" control="BOOST"/>
124   </propeller>
125
126   <gear x="2.043" y="1.468" z="-1.561" 
127         compression="0.3" 
128         retract-time="7" 
129         spring="1" 
130         damp="10">
131         <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
132         <control-input axis="/controls/gear/brake-left" control="BRAKE"/>
133         <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
134
135         <control-speed control="EXTEND" transition-time="7"/>
136
137         <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
138   </gear>
139
140   <gear x="2.043" y="-1.468" z="-1.561" 
141         compression="0.3" 
142         retract-time="7" 
143         spring="1" 
144         damp="10">
145         <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
146         <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
147         <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
148
149         <control-speed control="EXTEND" transition-time="7"/>
150
151         <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
152   </gear>
153
154   <!-- Tail wheel; has castering selectable by a wheel lock -->
155   <gear x="-4.068" y="0" z="-0.233" 
156         compression="0.2">
157
158         <control-input axis="/controls/gear/tailwheel-lock" src0="0" src1="1" dst0="1" dst1="0" control="CASTERING"/>
159   </gear>
160
161   <tank x="0" y="0.0" z="0.0" capacity="1000"/>
162
163   <!-- CH théorique x=1.312 y=0 z=-0.219 --> 
164   <ballast x="0.77" y="0.0" z="-0.065" mass="500"/>
165
166 </airplane>
167