-
Notifications
You must be signed in to change notification settings - Fork 1
/
Citation-II-yasim.xml
241 lines (203 loc) · 12.1 KB
/
Citation-II-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
<!-- http://www.aoc.noaa.gov/aircraft_cessna.htm -->
<!-- http://www.airliners.net/info/stats.main?id=160 -->
<!-- http://www.linkaviation.com/document/citation-training-manual%20.doc -->
<!-- http://www.avdex.co.za/performance/per00147.htm -->
<!-- empty equiped weight is 8060 lbs, max operating weight is 13700 -->
<!-- lbs, max fuel load is 5008 lbs (which is shouldn't be included in -->
<!-- the airplane mass number below. With a full fuel load, that -->
<!-- leaves 632 lbs remaining for other things like the pilots and -->
<!-- passengers and baggage. Load will be added at the end of this -->
<!-- config file using the <weight> tag -->
<!--Performance at 12000 lbs -->
<airplane mass="8060">
<approach speed="86" aoa="15" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-real" value="0.3"/>
<control-setting axis="/controls/engines/engine[1]/throttle-real" value="0.3"/>
<control-setting axis="/controls/engines/engine[0]/condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/condition" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="117"/>
<solve-weight idx="1" weight="169"/>
<solve-weight idx="2" weight="768"/>
<solve-weight idx="3" weight="0"/>
</approach>
<cruise speed="331" alt="36000" fuel="0.87"> <!-- 162 indicated -->
<control-setting axis="/controls/flight/elevator" value="0.0"/>
<control-setting axis="/controls/engines/engine[0]/throttle-real" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/throttle-real" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/condition" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="117"/>
<solve-weight idx="1" weight="169"/>
<solve-weight idx="2" weight="768"/>
<solve-weight idx="3" weight="0"/>
</cruise>
<!-- 15.9m (1674 pixels) wingspan, 105.28 pixels/meter -->
<!-- 0,0,0 ref point is at the nose -->
<!-- -X is towards the rear, +Y is left, +Z is up -->
<cockpit x="-3.17" y="0.31" z="0.95"/>
<!-- FUSELAGE -->
<fuselage ax="0" ay="0" az="0.02" bx="-2.838" by="0" bz="0.514"
width="1.60" taper="0.2" midpoint="1.0" idrag="1.2"/>
<fuselage ax="-2.838" ay="0" az="0.514" bx="-8.667" by="0" bz="0.514"
width="1.60" taper="1" midpoint="0.4" idrag="1.2"/>
<fuselage ax="-8.667" ay="0" az="0.514" bx="-13.656" by="0" bz="0.870"
width="1.60" taper="0.1" midpoint="0.0" idrag="1.2"/>
<!-- Engines -->
<fuselage ax="-8.016" ay="1.33" az="0.893" bx="-10.336" by="1.33" bz="0.893"
width="0.92" taper="0.5" midpoint="0.25" idrag="1.2"/>
<fuselage ax="-8.016" ay="-1.33" az="0.893" bx="-10.336" by="-1.33" bz="0.893"
width="0.92" taper="0.5" midpoint="0.25" idrag="1.2"/>
<!-- L.E.MAC = -6.177 / 25% = -6.679-->
<wing x="-7.0" y="0.87" z="-0.11" length ="7.10" chord ="2.77"
sweep="0" dihedral="4" taper="0.34" camber="0.0" incidence="2.5"
twist="-3.0">
<stall aoa="15" width="18" peak="1.5"/>
<flap0 start="0" end=".52" lift="1.5" drag="1.7"/>
<flap1 start=".52" end=".88" lift="1.2" drag="1.1"/>
<spoiler start="0.4" end="0.5" lift="1" drag="14.0"/>
<control-input control="FLAP0" axis="/controls/flight/flaps"/>
<control-speed control="FLAP0" transition-time="7"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input control="FLAP1" axis="/controls/flight/aileron" split="true"/>
<control-input control="FLAP1" axis="/controls/flight/aileron-trim" split="true"/>
<control-output control="FLAP1" prop="/surface-positions/left-aileron-pos-norm" side="left"/>
<control-output control="FLAP1" prop="/surface-positions/right-aileron-pos-norm" side="right"/>
<control-input control="SPOILER" axis="/controls/flight/speedbrake" />
<control-speed control="SPOILER" transition-time="1"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
</wing>
<!--
<wing x="-7.0" y="0.87" z="-0.11" length ="7.10" chord ="2.77"
sweep="0" dihedral="4" taper="0.34" camber="0.0" incidence="2.5"
twist="-3.0">
<stall aoa="15" width="18" peak="1.5"/>
<flap0 start="0" end=".52" lift="1.5" drag="1.7"/>
<flap1 start=".52" end=".88" lift="1.2" drag="1.1"/>
<flap2 start=".52" end=".70" lift="1.05" drag="1.02"/>
<spoiler start="0.4" end="0.5" lift="1" drag="14.0"/>
<control-input control="FLAP0" axis="/controls/flight/flaps"/>
<control-speed control="FLAP0" transition-time="7"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input control="FLAP1" axis="/controls/flight/aileron" split="true"/>
<control-output control="FLAP1" prop="/surface-positions/left-aileron-pos-norm" side="left"/>
<control-output control="FLAP1" prop="/surface-positions/right-aileron-pos-norm" side="right"/>
<control-input control="FLAP2" axis="/controls/flight/aileron-trim"/>
<control-output control="FLAP2" prop="/surface-positions/aileron-trim-pos-norm"/>
<control-input control="SPOILER" axis="/controls/flight/speedbrake" />
<control-speed control="SPOILER" transition-time="1"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
</wing>
-->
<hstab x="-12.64" y="0.05" z="1.48" length="2.88" chord="1.48"
sweep="0" dihedral="9" taper="0.53" camber="0.0">
<stall aoa="18" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.1"/>
<control-input control="FLAP0" axis="/controls/flight/elevator"/>
<control-input control="FLAP0" axis="/controls/flight/elevator-trim"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<!--
<hstab x="-12.64" y="0.05" z="1.48" length="2.88" chord="1.48"
sweep="0" dihedral="9" taper="0.53" camber="0.0">
<stall aoa="18" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.1"/>
<flap1 start="0.06" end="0.54" lift="1.1" drag="1.02"/>
<control-input control="FLAP0" axis="/controls/flight/elevator"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
<control-input control="FLAP1" axis="/controls/flight/elevator-trim"/>
<control-output control="FLAP1" prop="/surface-positions/elevator-trim-pos-norm"/>
</hstab>
-->
<vstab x="-12.43" y="0.00" z="1.03" length="2.60" chord="2.48"
sweep="26.5" taper="0.46">
<stall aoa="16" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<flap1 start="0.20" end="0.43" lift="1.04" drag="1.02"/>
<control-input control="FLAP0" axis="/controls/flight/rudder" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-input control="FLAP1" axis="/controls/flight/rudder-trim" invert="true"/>
<control-output control="FLAP1" prop="/surface-positions/rudder-trim-pos-norm"/>
</vstab>
<!-- 2 wet wing tanks 371 US gallons, ~366 US gallons usable each.
If using Jet A (6.84 lbs/gal) 2537.64lbs, 2504lbs usable
If using Jet A-1 (6.72 lbs/gal), 2493.12lbs, 2460lbs usable
Here we must specify the full weight, not the usable weight.
See Citation-II-set.xml for the unusable capacity.
-->
<tank x="-7.18" y="1.5" z="0.0" capacity="2493.12" jet="true"/>
<tank x="-7.18" y="-1.5" z="0.0" capacity="2493.12" jet="true"/>
<tank x="-7.18" y="0" z="0" capacity="0"/>
<gear x="-1.76" y="0.00" z="-0.9355" compression=".2" retract-time="7" sfric="0.99">
<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>
<gear x="-7.20" y="2.68" z="-0.9266" compression=".2" retract-time="7"
sfric="0.9" dfric="0.9">
<control-input axis="/controls/gear/brake-left-real" 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="6.2"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
</gear>
<gear x="-7.20" y="-2.68" z="-0.9266" compression=".2" retract-time="7"
sfric="0.9" dfric="0.9">
<control-input axis="/controls/gear/brake-right-real" 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="6"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
</gear>
<!-- Pratt and Whitney Canada Inc. JT15D-4 Turbofan -->
<!-- The real-life values for n1-max and n2-max are 104% and 96%
respectively but YASim does not neem to provide a very accurate
simulation. Here we use numbers tweaked to provide 104% and 96%
at full throttle during cruise, and 2500 pounds-force of thrust
at 104%, sea level and 0 knots. -->
<jet x="-9.19" y="1.37" z="0.76" mass="519" thrust="2635.6" tsfc="0.562" egt="973.15"
n1-idle="45" n1-max="107.2" n2-idle="49.0" n2-max="99.8" spool-time="2.5" epr="2.7">
<control-input axis="/controls/engines/engine[0]/throttle-real" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser-real" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-10.5" y="1.37" z="0.76"/>
</jet>
<jet x="-9.19" y="-1.37" z="0.76" mass="519" thrust="2635.6" tsfc="0.562" egt="973.15"
n1-idle="45" n1-max="107.2" n2-idle="49.0" n2-max="99.8" spool-time="2.5" epr="2.7">
<control-input axis="/controls/engines/engine[1]/throttle-real" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser-real" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-10.5" y="-1.37" z="0.76"/>
</jet>
<!-- The <ballast> tag doesn't add weight, but instead specifies the -->
<!-- distribution of the overall weight. -->
<!-- target CG is about -6.76 -->
<ballast x="-12.43" y="0.0" z="2" mass="-1000"/>
<ballast x="-12.64" y="0.0" z="1.48" mass="-1000"/>
<!-- Pushback -->
<thruster x="-1.76" y="0.00" z="-0.74" vx="1" vy="0" vz="0" thrust="1500">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1" />
</thruster>
<!-- The <weight> tags add weight over and above the aircraft empty -->
<!-- weight and fuel weight. The sum of these values can be anything -->
<!-- in the range of 0 to 10400 (max weight) minus 5722 (empty weight) -->
<!-- minus fuel load. I.e. the remaining available load for safe -->
<!-- flying. So if fuel fraction is 0.8, this sum can be in the range -->
<!-- of 0 to (10400 - 5722 - 1920 = 2758.) 0 of course would mean -->
<!-- ghost pilots, so it should be a bit more than that. -->
<!-- You can double check total gross weight at flight time by looking -->
<!-- at /yasim/gross-weight-lbs in the property tree. It should not ever -->
<!-- exceed 10400 lbs. -->
<!-- the /yasim/beech99/*-lbs propertis are initialized in the -->
<!-- beech99-yasim-set.xml file and can be adjusted at run time. -->
<weight x="-2.0" y="0" z="-0.5" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="-4.0" y="0" z="-0.5" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="-6.7" y="0" z="-0.5" mass-prop="/sim/weight[2]/weight-lb"/>
<weight x="-9.0" y="0" z="-0.5" mass-prop="/sim/weight[3]/weight-lb"/>
</airplane>