-
Notifications
You must be signed in to change notification settings - Fork 0
/
Copy pathf22-yasim.xml
318 lines (269 loc) · 12.9 KB
/
f22-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
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
<!--
=========================================
AeroFab - 2010 - Lockheed-Martin-FA-22A-Raptor Project
=========================================
http://aerofab.webnode.pt/
Creation : April 15, 2010 06:33:00 PM
Last update: November 10, 2010 07:41:02 PM
Revisions :
* October 1, 2010 04:27:45 PM
* November 10, 2010 07:41:02 PM ()
======================================================================
Contributions :
Fabrizio Fracaroli <[email protected] >
======================================================================
/*
* Copyright (c) 2010 Fabrizio Fracaroli <[email protected] >
*
* This file is free software: you may copy, redistribute and/or modify it
* under the terms of the GNU General Public License as published by the
* Free Software Foundation, either version 2 of the License.
*
* This file is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
* General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with this program. If not, see http://www.gnu.org/licenses/ .
*
* This file incorporates work covered by the following copyright and
* permission notice:
*
* Copyright 2010, Fabrizio Fracaroli <[email protected] >
*
* Permission to use, copy, modify, and/or distribute this software
* for any purpose with or without fee is hereby granted, provided
* that the above copyright notice and this permission notice appear
* in all copies.
* THE SOFTWARE IS PROVIDED "AS IS" AND THE AUTHOR DISCLAIMS ALL
* WARRANTIES WITH REGARD TO THIS SOFTWARE INCLUDING ALL IMPLIED
* WARRANTIES OF MERCHANTABILITY AND FITNESS. IN NO EVENT SHALL THE
* AUTHOR BE LIABLE FOR ANY SPECIAL, DIRECT, INDIRECT, OR
* CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER RESULTING FROM LOSS
* OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF CONTRACT,
* NEGLIGENCE OR OTHER TORTIOUS ACTION, ARISING OUT OF OR IN
* CONNECTION WITH THE USE OR PERFORMANCE OF THIS SOFTWARE.
*/
======================================================================
Reference :
http://en.wikipedia.org/wiki/ -->
<airplane mass="43430">
<!-- Approach configuration -->
<approach speed="145" aoa="8" fuel="1">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<control-setting axis="/controls/flight/speedbrake" value="1"/>
<control-setting axis="/controls/flight/slats" value="1"/>
</approach>
<!-- Cruise configuration. -->
<cruise speed="1500" alt="45000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.9"/>
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.9"/>
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="0"/>
</cruise>
<!-- pilot eyepoint -->
<cockpit x="4.47138" y="0" z="-0.016786"/>
<!-- fuselage -->
<fuselage ax="9.46348" ay="0" az="-1.12311"
bx="5.09406" by="0" bz="-0.660128"
width="1.79" taper= "0" midpoint= "1" />
<fuselage ax="5.09406" ay="0" az="-0.660128"
bx="-7.61961" by="0" bz="-0.721073"
width="1.79" taper= "0.5" midpoint= "0" />
<wing x="-2.81409" y="2.26033" z="-0.581897"
length="4.5"
chord="7.5"
taper="0.24"
sweep="22"
dihedral="0"
camber="0.1"
incidence="2.0"
twist="-2.0">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.0" end="1" lift="1.2" drag="2"/>
<flap1 start="0.47" end="0.8" lift="1.2" drag="1.2"/>
<slat aoa="4" start="0.1" end="0.813" lift="1.5" drag="1.3"/>
<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/flaps" control="SLAT"/>
<control-output control="FLAP0" prop="/surface-positions/left-flap-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/right-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="SLAT" prop="/surface-positions/slat-pos-norm"/>
<control-speed control="SLAT" transition-time="1.1"/>
<control-speed control="FLAP0" transition-time="1.5"/>
<control-speed control="FLAP1" transition-time="1.5"/>
</wing>
<mstab x="-2.81409" y="2.26033" z="-0.581897"
length="4.5"
chord="7.5"
taper="0.24"
sweep="22"
dihedral="0"
camber="0.1"
incidence="2.0"
twist="-2.0">
<flap0 start="0.0" end="0.5" lift="0.25" drag="2"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="3.0"/>
</mstab>
<hstab x="-7.17643" y="2.10165" z="-0.459948"
taper="0.3"
length="2.51"
chord="3.96"
sweep="30"
dihedral="0"
camber="-0.01"
effectiveness="2.0">
<stall aoa="40.0" width="2" peak="1.2"/>
<flap0 start="0" end="1" lift="1.5" drag="1"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP1"/>
<control-output control="FLAP0" side="left" prop="/surface-positions/left-taileron-pos-norm"/>
<control-output control="FLAP0" side="right" prop="/surface-positions/right-taileron-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/taileron-pos-norm"/>
<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="FLAP1" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
<control-speed control="FLAP1" transition-time="3.0"/>
</hstab>
<vstab x="-5.03725" y="1.42478" z="-0.461207"
taper="0.32"
length="3.1"
chord="4.443"
dihedral="65"
sweep="0" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="0.8"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" 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="1"/>
</vstab>
<vstab x="-5.03725" y="-1.42478" z="-0.461207"
taper="0.32"
length="3.1"
chord="4.443"
dihedral="115"
sweep="0" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="0.8"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" 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="1"/>
</vstab>
<!--The vectors should be setting to more than 20 degrees for a really vertical climb. I think
If the vectors would be setting to more than 20 degrees You must to change this (src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR")
as this example If you increase the vectors for example 10 degrees so you must to decrease (src0="-0.75") minus 10 degress so it will be like this
(src0="-0.65" dst0="0.0" src1="1" dst1="1.0" control="VECTOR") SRC0="minus zero dot six five (pay attention)
If dont, the animation of the vectors will be wrong
PM for me if you have doubt -->
<jet x="-3.85632" y="-0.65189" z="-0.716246"
mass="3900"
thrust="23500"
afterburner="35000"
n1-idle="55"
n1-max="100"
n2-idle="55"
n2-max="105"
exhaust-speed="1550"
tsfc="0.7"
rotate="20">
<actionpt x="-7.99144" y="-0.65189" z="-0.716246"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.0" dst0="0.0" src1="0.86" dst1="1.0" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.88" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-input axis="/controls/flight/elevator" src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR"/>
<control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
<control-output control="VECTOR" prop="/engines/engine[0]/vector-norm" min="-1" max="1"/>
<control-speed control="THROTTLE" transition-time="3.0"/>
<control-speed control="REHEAT" transition-time="8.0"/>
</jet>
<jet x="-3.85632" y="0.65189" z="-0.716246"
mass="3900"
thrust="23500"
afterburner="35000"
n1-idle="55"
n1-max="100"
n2-idle="55"
n2-max="105"
exhaust-speed="1550"
tsfc="0.7"
rotate="20">
<actionpt x="-7.99144" y="0.65189" z="-0.716246"/>
<control-input axis="/controls/engines/engine[1]/throttle" src0="0.0" dst0="0.0" src1="0.86" dst1="1.0" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/throttle" src0="0.88" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-input axis="/controls/flight/elevator" src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR"/>
<control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
<control-output control="VECTOR" prop="/engines/engine[1]/vector-norm" min="-1" max="1"/>
<control-speed control="THROTTLE" transition-time="3.0"/>
<control-speed control="REHEAT" transition-time="8.0"/>
</jet>
<!-- gear -->
<!-- nose -->
<gear x="3.00181" y="0" z="-2.80013"
retract-time="8"
compression="0.5" spring="0.5" upx="0" upy="0" upz="0.3">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- left main -->
<gear x="-2.49889" y="2.10045" z="-2.80013"
retract-time="8"
compression="0.2"
spring="0.8"
damp="3">
<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-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-output control="BRAKE" prop="/gear/gear[1]/brake-position-norm"/>
<control-speed control="EXTEND" transition-time="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- right main -->
<gear x="-1.521" y="-2.10045" z="-2.80013"
retract-time="8"
compression="0.2"
spring="0.8" damp="3">
<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-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-output control="BRAKE" prop="/gear/gear[2]/brake-position-norm"/>
<control-speed control="EXTEND" transition-time="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<tank x="3.0232" y="0" z="-0.684553" jet="true" capacity="6500"/>
<tank x="1.01233" y="0" z="-0.641769" jet="true" capacity="3500"/>
<!-- left wing tank -->
<tank x="-2.02343" y="3.7483" z="-0.484877" jet="true" capacity="4000"/>
<!-- right wing tank -->
<tank x="-2.02343" y="-3.7483" z="-0.484877" jet="true" capacity="4000"/>
<ballast x="4.56742" y="0" z="-0.684553" mass ="2650"/>
<ballast x="1.78245" y="0" z="-0.94126" mass ="5000"/>
<ballast x="7.40563" y="0" z="-0.810242" mass ="1995"/>
</airplane>