forked from ranguli/dhc6
-
Notifications
You must be signed in to change notification settings - Fork 0
/
dhc6pF.xml
306 lines (264 loc) · 15.5 KB
/
dhc6pF.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
<?xml version="1.0" encoding="UTF-8"?>
<!--
DHC6-300 Twin Otter
Jan 2008 by Syd Adams.
SPECS:
Height: 5.9m
Length: 15.77
Wing span: 19.8
MTOW: 12,500 lbs
Service Ceiling = 26700 ft
Cruise at MTOW
5000 ft - 181 TAS
10,000 ft - 182 TAS
Stall :
Full Flaps = 58 kt
O Flaps = 74 kt
-->
<airplane mass="7500" version="YASIM_VERSION_CURRENT">
<approach speed="78" aoa="6.0" fuel="0.5">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3150"/>
</approach>
<cruise speed="172" alt="10000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3350"/>
</cruise>
<cockpit x="2.8" y="0.3" z="0.745"/>
<fuselage ax="6.338" ay="0" az="-0.185" bx="3.609" by="0" bz="0.111"
width="1.8" taper="0.2" midpoint="1.0" cy="1.1" cx="1.1"/>
<fuselage ax="3.609" ay="0" az="0.111" bx="-2.470" by="0" bz="0.111"
width="1.8" taper="1.0" midpoint="0.5" cy="1.1" cx="1.1" />
<fuselage ax="-2.470" ay="0" az="0.111" bx="-8.811" by="0" bz="0.30"
width="1.8" taper="0.1" midpoint="0.0" cy="1.1" cx="1.1" />
<fuselage ax="2.497" ay="2.857" az="0.858" bx="-0.410" by="2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<fuselage ax="2.497" ay="-2.857" az="0.858" bx="-0.410" by="-2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<wing x="0.0" y="0.80" z="1.0" length="9.0" chord="2.0"
sweep="0" dihedral="3" taper="1" incidence="2.5" idrag="1.0" camber="0.24">
<stall aoa="10" width="6" peak="1.5"/>
<flap0 start="0" end="0.90" lift="1.6" drag="3.2"/>
<flap1 start="0.6" end="0.90" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-speed control="FLAP0" transition-time="20"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<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"/>
</wing>
<hstab x="-7.47" y="0.08" z="1.186" length="3.15" chord="1.4"
sweep="0" dihedral="0" taper="1" camber="-0.05">
<stall aoa="17" width="6" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="1.5"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-7.312" y="0.00" z="0.3" length="2.6" chord="2.9"
sweep="20" taper="0.7" >
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<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"/>
</vstab>
<!-- frt doors-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LF-door/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LF-door/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RF-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RF-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear doors pasenger-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-F/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-F/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RR-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RR-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear door baggage -->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-R/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-R/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/Baggage-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/Baggage-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!--
2500 lbs (Jet A)
Fuel burn ... 580 lbs/hr
-->
<tank x="0.66" y="0" z="-0.5" capacity="1000" jet="true"/>
<tank x="-1.32" y="0" z="0.5" capacity="1400" jet="true"/>
<tank x="0" y="0" z="0" capacity="0"/>
<!-- Floats-->
<gear x="3.758" y="1.75" z="-2.2" compression="1.5" spring = "15" sfric = "1.2" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.5"
speed-planing="15" spring-factor-not-planing="0.3">
</gear>
<gear x="3.758" y="-1.75" z="-2.2" compression="1.5" spring = "15" sfric = "1.2" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.5"
speed-planing="15" spring-factor-not-planing="0.3">
</gear>
<gear x="-2.2" y="1.75" z="-1.7" compression="1.5" spring = "15" sfric = "1.4" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.2"
speed-planing="25" spring-factor-not-planing="0.25">
</gear>
<gear x="-2.2" y="-1.75" z="-1.7" compression="1.5" spring = "15" sfric = "1.4" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.2"
speed-planing="25" spring-factor-not-planing="0.25">
</gear>
<!-- Retractable wheels-->
<gear x="4.9" y="1.75" z="-2.744" compression="0.4" spring = "2" sfric = "0.5" dfric=".45" retract-time="4" initial-load="0" damp="0.6">
<control-input control="STEER" axis="/controls/gear/tiller" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="4.9" y="-1.75" z="-2.744" compression="0.4" spring = "2" sfric = "0.5" dfric=".45" retract-time="4" initial-load="0" damp="0.6">
<control-input control="STEER" axis="/controls/gear/tiller" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[5]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="-1.26" y="1.75" z="-2.68" compression="0.4" spring = "3.5" sfric = "0.5" dfric=".45" retract-time="4" initial-load="1" damp="10.1">
<control-input control="BRAKE" axis="/controls/gear/brake-parking" />
<control-input control="BRAKE" axis="/controls/gear/brake-left" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[6]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="-1.26" y="-1.75" z="-2.68" compression="0.4" spring = "3.5" sfric = "0.5" dfric=".45" retract-time="4" initial-load="1" damp="10.1">
<control-input control="BRAKE" axis="/controls/gear/brake-parking" />
<control-input control="BRAKE" axis="/controls/gear/brake-right" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[7]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<!-- 2 more Floats, need to be at this position in the file to do not brake the animation
"reduce-friction-by-extension" is reduced to get steering control-->
<gear x="-4.2" y="1.75" z="-1.7" compression="1.8" spring = "8" sfric = "0.9" dfric = "0.8" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="0.7"
speed-planing="25" spring-factor-not-planing="3">
<control-input axis="/controls/gear/tiller" control="STEER"
invert ="true" square="true"/>
</gear>
<gear x="-4.2" y="-1.75" z="-1.7" compression="1.8" spring = "8" sfric = "0.9" dfric = "0.8" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="0.7"
speed-planing="25" spring-factor-not-planing="3">
<control-input axis="/controls/gear/tiller" control="STEER"
invert="true" square="true"/>
</gear>
<!-- The Floats on solid ground-->
<gear x="3.75" y="1.75" z="-2.2" compression="0.4" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="3.75" y="-1.75" z="-2.2" compression="0.4" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="-4.2" y="1.75" z="-1.70" compression="0.2" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="-4.2" y="-1.75" z="-1.7" compression="0.2" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<!-- Retractable wheels on water-->
<gear x="0" y="1.75" z="-2.2" compression="0.2" spring = "0.1" sfric = "1" dfric="1" retract-time="4" on-water="1" on-solid="0"
ignored-by-solver="1" reduce-friction-by-extension="0.5">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="0" y="-1.75" z="-2.2" compression="0.2" spring = "0.1" sfric = "1" dfric ="1" retract-time="4" on-water="1" on-solid="0"
ignored-by-solver="1" reduce-friction-by-extension="0.5">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<!--
Engines:
2 PT6A-34
750 shp
Prop diam: 2.59 m
-->
<propeller x="1.3" y="2.65" z="1.0"
mass="500" moment="40" radius="1.1"
cruise-speed="146" cruise-rpm="1650"
cruise-power="375" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="750" eng-rpm="2110" alt="0"
flat-rating="750" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[0]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[0]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[0]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[0]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<propeller x="1.3" y="-2.65" z="1.1"
mass="500" moment="40" radius="1.0"
cruise-speed="146" cruise-rpm="1650"
cruise-power="375" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="750" eng-rpm="2110" alt="0"
flat-rating="750" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="-2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[1]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[1]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[1]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[1]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<thruster x="2.2" y="2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[0]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[0]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<thruster x="2.2" y="-2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[1]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[1]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<weight x="2.5" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.0" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<ballast x="5" y="0" z="-2.5" mass="2078"/>
<hitch name="aerotow" x="-2.5" y="0" z="-0.85" force-is-calculated-by-other="1">
<tow length="60" weight-per-meter="0.035" elastic-constant="9000" break-force="10000" mp-auto-connect-period="1.0"/>
<winch max-tow-length="1000" min-tow-length="60" initial-tow-length="60"/>
</hitch>
</airplane>