forked from l0k1/A-10
-
Notifications
You must be signed in to change notification settings - Fork 0
/
A-10-yasim.xml
261 lines (229 loc) · 11.6 KB
/
A-10-yasim.xml
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
<!-- A-10 yasim config. This is a hack and not an authentic
representation of the aircraft. Having said that, the
numbers, where I could find them, roughly match those of
the original aircraft.
Lee Elliott.
-->
<!--
Aircraft mass comprises pilot, oxygen, unusable fuel & oil, gun and
six pylons. The solve weight used in the approach and cruise
configurations represent a full ammunition load (1350 x 2lbs)
-->
<airplane mass="24959">
<!-- Approach configuration -->
<approach speed="120" aoa="8" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/controls/flight/spoilers" value="0.5"/>
<control-setting axis="/controls/gear/gear-down" value="1.0"/>
<solve-weight idx="0" weight="2700"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="380" alt="15000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/flight/spoilers" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0.0"/>
<solve-weight idx="0" weight="2700"/>
</cruise>
<cockpit x="-3.25" y="0.0" z="1.2"/>
<fuselage ax="0" ay="0" az="0" bx="-16.16" by="0" bz="0"
width="1.4" taper="0.9"/>
<!-- Left Engine -->
<fuselage ax="-9.44" ay="1.50" az="1.3" bx="-12.73" by="1.50" bz="1.18"
width="1.5"/>
<!-- Right Engine -->
<fuselage ax="-9.44" ay="-1.50" az="1.3" bx="-12.73" by="-1.50" bz="1.18"
width="1.5"/>
<wing x="-8.32" y="0.63" z="0.0" taper="0.7" incidence="-0.8"
length="8.31" chord="3.23" sweep="0.0" dihedral="3.0"
camber="0.0" twist="-1">
<stall aoa="15" width="6" peak="1.3"/>
<flap0 start="0.04" end="0.51" lift="1.3" drag="1.3"/>
<flap1 start="0.54" end="0.86" lift="1.6" drag="1.3"/>
<spoiler start="0.54" end="0.86" lift="0.6" drag="10.0"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
<control-output control="FLAP0" side="left"
prop="/surface-positions/left-flap-pos-norm"/>
<control-output control="FLAP0" side="right"
prop="/surface-positions/right-flap-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP1" side="left"
prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right"
prop="/surface-positions/right-aileron-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
<control-output control="SPOILER" side="left"
prop="/surface-positions/left-spoiler-pos-norm"/>
<control-output control="SPOILER" side="right"
prop="/surface-positions/right-spoiler-pos-norm"/>
<control-output control="SPOILER" prop="/surface-positions/spoiler-pos-norm"/>
<control-speed control="FLAP0" transition-time="15"/>
<control-speed control="FLAP1" transition-time="0.5"/>
<control-speed control="SPOILER" transition-time="1.0"/>
</wing>
<hstab x="-14.88" y="0.42" z="0.41" taper="0.0" effectiveness="2"
length="2.38" chord="1.95" sweep="0.0" dihedral="0.0"
camber="-0.0">
<stall aoa="15" width="3" peak="1.3"/>
<flap0 start="0" end="1" lift="1.8" drag="1.7"/>
<control-input axis="sim/model/A-10/controls/flight/sas-elevator" control="FLAP0"
square="true"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" side="left"
prop="surface-positions/left-elevator-pos-norm"/>
<control-output control="FLAP0" side="right"
prop="surface-positions/right-elevator-pos-norm"/>
<control-output control="FLAP0" prop="surface-positions/elevator-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.2"/>
</hstab>
<vstab x="-14.88" y="2.85" z="0.0" taper="0.6" effectiveness="2"
length="2.8" chord="2.14" sweep="0.0">
<stall aoa="16" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.5"/>
<control-input axis="/controls/flight/rudder" control="FLAP0"
square="true" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0"
invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
</vstab>
<vstab x="-14.88" y="-2.85" z="0.0" taper="0.6" effectiveness="2"
length="2.8" chord="2.14" sweep="0.0">
<stall aoa="16" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.5"/>
<control-input axis="/controls/flight/rudder" control="FLAP0"
square="true" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0"
invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
</vstab>
<!-- 2 x GE TF34-100 -->
<!-- GE TF34-100 characteristics:
thrust (at sea level): 9065 lbs (40422 N)
weight: 1,458 lbs
fuel consumption: 0.363 lbs per pound of thrust
bypass ratio: 6.42
pressure ratio: 21
fan/core thrust ratio: 0.85
spool time (idle to 100%): 10 sec
fan airflow: 338 lb/sec
fan airflow speed: 223.6 m/s (=> 434.64 kt) ( Vo(m/s)-Vi(m/s)=Thrust(N)/Dm(Kg/s) => (40422*0.85)/(338/2.2) , at takeoff we consider Ve = 0)
fan speed: 7,365 rpm
compressor airflow: 47 lb/sec
compressor airflow speed: 283.8 m/s (=> 551.7 kt)
compressor speed: 17,900 rpm
exhaust gas temperature: 813 °C
-->
<jet x="-10.8" y="1.5" z="1.27" mass="1440" thrust="9065" spool-time="8" tsfc="0.371" n1-idle="20" n1-max="100" n2-idle="56" n2-max="102" epr="1.42" egt="1086" rotate="9">
<actionpt x="-12.5" y="1.5" z="1.15"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
</jet>
<jet x="-10.8" y="-1.5" z="1.27" mass="1440" thrust="9065" spool-time="8" tsfc="0.371" n1-idle="20" n1-max="100" n2-idle="56" n2-max="102" epr="1.42" egt="1086" rotate="9">
<actionpt x="-12.5" y="-1.5" z="1.15"/>
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
</jet>
<!-- Internal tanks -->
<tank x="-8.3" y="2.0" z="0.0" jet="true" capacity="2089.92"/><!-- ppg=6.72, real tank capacity : 311 gallons -> 311*6.72 = 2089.92 lbs -->
<tank x="-8.8" y="0.0" z="0.63" jet="true" capacity="3433.92"/><!-- real tank capacity: 511 gallons -> 511*6.72 = 3433.92 lbs -->
<tank x="-7.2" y="0.0" z="0.63" jet="true" capacity="3433.92"/>
<tank x="-8.3" y="-2.0" z="0.0" jet="true" capacity="2089.92"/>
<!-- Ferry Tanks -->
<tank x="-7.6" y="1.29" z="-0.86" jet="true" capacity="4032"/> <!-- 600*6.72 = 4032 -->
<tank x="-7.6" y="0" z="-0.86" jet="true" capacity="4032"/>
<tank x="-7.6" y="-1.29" z="-0.86" jet="true" capacity="4032"/>
<!-- Undercarriage -->
<!-- nose -->
<gear x="-2.85" y="0.4" z="-2.33" compression="0.30" spring="0.25" damp="1.4">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
</gear>
<!-- left main -->
<gear x="-8.3" y="2.5" z="-2.37" compression="0.4" spring="0.25" damp="1.4">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="gear/gear[1]/position-norm"/>
</gear>
<!-- right main -->
<!--<gear x="-8.3" y="-2.5" z="-2.22" retract-time="6" compression="0.7" spring="1.6" damp="1.4">-->
<gear x="-8.3" y="-2.5" z="-2.37" compression="0.4" spring="0.25" damp="1.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
</gear>
<!-- Ballast -->
<ballast x="-3.16" y="0" z="0.78" mass="1200" /><!-- Titanium bathtub (for the mass see: http://www.plane-crazy.net/links/a10.htm) -->
<ballast x="-1.71" y="0.183" z="-0.823" mass="620"/><!-- GAU-8 barrel (length: 2800mm + 620mm) -->
<ballast x="-4.91" y="0" z="0" mass="2310"/><!-- GAU-8 feed system + ammunition drum + aluminium alloy cases + plastic driving bands -->
<ballast x="-6.1" y="0" z="0.0" mass="1000"/> <!-- avionics -->
<ballast x="-4" y="0" z="0.0" mass="2500"/> <!-- CG trim trim -->
<!--
GAU-8/A characteristics:
Magazine capacity: 1,350 max (1,174 is the normal load)
Rate of fire: 3900 RPM
Barrel length: 2.80 m
Total length: 6.4 m (from the muzzle to the rearmost point of the ammunition system)
Barrel weight: 620 lb
Total weight: 4,029 lb (complete weapon + ammunition load)
Recoil force: 10,000 lb
Ammo types:
PGU-14/B API: Armor Piercing Incendiary (with depleted uranium)
projectile weight: 425 grams
velocity: 3250 ft/sec
PGU-13/B HEI: High Explosive Incendiary
projectile weight: 360 grams
velocity: 3425 ft/sec
Note: The standard ammunition mixture for anti-armor use is a four-to-one mix of PGU-14/B and PGU-13/B rounds.
-->
<weight x="-4.91" y="0" z="0.0" size="0" mass-prop="yasim/weights/ammunition-weight-lbs"/>
<!-- Stations, weight is dynamicly configured while choosing the weapons,
drag should be too, but it's not possible yet in YASim-->
<weight x="-7.56" y="5.90" z="0.00"
size="0.25"
mass-prop="sim/weight[0]/weight-lb"/><!-- #1 extern L-->
<weight x="-7.56" y="4.83" z="-0.22"
size="0.25"
mass-prop="sim/weight[1]/weight-lb"/>
<weight x="-7.56" y="3.62" z="-0.37"
size="0.25"
mass-prop="sim/weight[2]/weight-lb"/>
<weight x="-7.56" y="1.69" z="-0.44"
size="0.25"
mass-prop="sim/weight[3]/weight-lb"/>
<weight x="-7.56" y="0.56" z="-0.44"
size="0.25"
mass-prop="sim/weight[4]/weight-lb"/><!--fuse L-->
<weight x="-7.56" y="0.00" z="-0.44"
size="0.25"
mass-prop="sim/weight[5]/weight-lb"/><!--center-->
<weight x="-7.56" y="-0.56" z="-0.44"
size="0.25"
mass-prop="sim/weight[6]/weight-lb"/><!--fuse R-->
<weight x="-7.56" y="-1.69" z="-0.44"
size="0.25"
mass-prop="sim/weight[7]/weight-lb"/>
<weight x="-7.56" y="-3.62" z="-0.37"
size="0.25"
mass-prop="sim/weight[8]/weight-lb"/>
<weight x="-7.56" y="-4.83" z="-0.22"
size="0.25"
mass-prop="sim/weight[9]/weight-lb"/>
<weight x="-7.56" y="-5.9" z="0.00"
size="0.25"
mass-prop="sim/weight[10]/weight-lb"/><!-- #11 extern R-->
<weight x="-7.56" y="-5.9" z="0.00"
size="0.25"
mass-prop="sim/weight[11]/weight-lb"/><!-- #11 extern R-->
</airplane>