-
Notifications
You must be signed in to change notification settings - Fork 0
/
Copy path747SP.xml
230 lines (199 loc) · 11.5 KB
/
747SP.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
<!--747-8 Intercontinental yasim
Specs:
4 - 67,400 lb GEnx-2B67 turbofans
Typical Cruise = 0.855 Mach / 35000 ft
Max Speed = 0.92 / 35000 ft
Wing span: 68.5 m
Length: 76.3 m
Tail Height: 19.4m
Diameter : 6.49
Wing Area: 524.90 m2
Max Fuel : 63034 US gal
Max TO weight: 987,000 lbs
TO speed : 180 kt
Landing speed : 155 kt
Mach 1 = 579 kt @ 35,000 ft
Leading edge MAC = 0.060 m
http://www.boeing.com/commercial/aeromagazine/articles/2010_q3/2/
-->
<airplane version="YASIM_VERSION_32" mass="485300">
<!-- Approach Configuration -->
<approach speed="151" aoa="3.6" fuel="0.1">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.3"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.3"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="400"/>
<solve-weight idx="1" weight="110000"/>
</approach>
<!-- Cruise Specifications -->
<cruise speed="516" alt="35000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.75"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="400"/>
<solve-weight idx="1" weight="110000"/>
</cruise>
<!-- Estimated using the 3d model -->
<cockpit x="28.106" y="0.0" z="3.313"/>
<!-- Fuselage -->
<fuselage ax="33.80000" ay="0.0" az="0.94" bx="26.17296" by="0.0" bz="1.82"
cx="1.0" cy="1.0" cz="0.83" width="7.825" taper="0.1" midpoint="1.0"/>
<fuselage ax="26.17296" ay="0.0" az="1.82" bx="10.91890" by="0.0" bz="1.82"
cx="1.0" cy="1.0" cz="0.83" width="7.825" taper="1.0" midpoint="0.5"/>
<fuselage ax="10.91890" ay="0.0" az="1.82" bx="-0.52165" by="0.0" bz="0.94"
cx="1.0" cy="1.0" cz="0.83" width="7.825" taper="0.8" midpoint="0.0"/>
<fuselage ax="-0.52165" ay="0.0" az="0.94" bx="-15.77571" by="0.0" bz="0.94"
cx="1.0" cy="1.0" cz="1.0" width="6.50" taper="1.0" midpoint="1.0"/>
<fuselage ax="-15.77571" ay="0.0" az="0.94" bx="-40.43781" by="0.0" bz="3.2"
cx="1.0" cy="1.0" cz="1.0" width="6.50" taper="0.2" midpoint="0.0"/>
<!-- Wings -->
<wing x="3.93180" y="3.2520" z="-0.98689" length="39.021" chord="12.414" sweep="37.5"
taper="0.23" dihedral="12.5" camber="0.08" incidence="2.4" twist="-1.8" idrag="1.2">
<stall aoa="12.0" width="5.0" peak="2.0"/>
<flap0 start="0" end="0.63" lift="1.8" drag="1.2"/>
<flap1 start="0.64" end="1.0" lift="1.7" drag="1.8"/>
<slat start="0" end="1" aoa="2" drag="1.1"/>
<spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/>
<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/slats" control="SLAT"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>
<control-speed control="SPOILER" transition-time="5"/>
<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-speed control="FLAP0" transition-time="120"/>
</wing>
<!-- Horizontal Stabilizer - Elevator -->
<hstab x="-33.94775" y="1.44144" z="3.58232" chord="8.20" length="10.80" taper="0.31"
sweep="28" dihedral="7" camber="-0.1" effectiveness="2.3">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.3"/>
<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>
<!-- Vertical Stabilizer - Rudder -->
<vstab x="-32.84332" y="0.00" z="3.58232" chord="14.315" length="16.166" taper="0.32"
sweep="45">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="0.9" lift="1.4" drag="1.3"/>
<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"
min="1" max="-1"/>
</vstab>
<!-- Engine Nacelles -->
<fuselage ax="-1.92155" ay="21.0366" az="-1.6768" bx="-8.18155" by="21.0366" bz="-1.6768"
cx="0.3" cy="1.0" cz="1.0" width="2.85" taper="0.75" midpoint="0.0"/>
<fuselage ax="6.71666" ay="11.8394" az="-2.8455" bx="0.45666" by="11.8394" bz="-2.8455"
cx="0.3" cy="1.0" cz="1.0" width="2.85" taper="0.75" midpoint="0.0"/>
<fuselage ax="6.71666" ay="-11.8394" az="-2.8455" bx="0.45666" by="-11.8394" bz="-2.8455"
cx="0.3" cy="1.0" cz="1.0" width="2.85" taper="0.75" midpoint="0.0"/>
<fuselage ax="-1.92155" ay="-21.0366" az="-1.6768" bx="-8.18155" by="-21.0366" bz="-1.6768"
cx="0.3" cy="1.0" cz="1.0" width="2.85" taper="0.75" midpoint="0.0"/>
<!-- Engines -->
<jet x="-2.17925" y="21.0366" z="-1.6768" mass="12400" thrust="67400"
egt="840" tsfc="0.34" exhaust-speed="1455.0">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-7.18" y="21.0366" z="-1.6768"/>
</jet>
<jet x="6.83465" y="11.8394" z="-2.8455" mass="12400" thrust="67400"
egt="840" tsfc="0.34" exhaust-speed="1455.0">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="1.46" y="11.8394" z="-2.8455"/>
</jet>
<jet x="6.83465" y="-11.8394" z="-2.8455" mass="12400" thrust="67400"
egt="840" tsfc="0.34" exhaust-speed="1455.0">
<control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[2]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[2]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="1.46" y="-11.8394" z="-2.8455"/>
</jet>
<jet x="-2.17925" y="-21.0366" z="-1.6768" mass="12400" thrust="67400"
egt="840" tsfc="0.34" exhaust-speed="1455.0">
<control-input axis="/controls/engines/engine[3]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[3]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[3]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-7.18" y="-21.0366" z="-1.6768"/>
</jet>
<!-- Pushback -->
<thruster x="19.28" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="25000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- ========================================================================================== -->
<!-- +==============+ -->
<!-- + LANDING GEAR + -->
<!-- +==============+ -->
<!-- Nosegear -->
<gear x="26.05101" y="0.0" z="-5.625" compression="0.25" spring="0.7" damp="4" sfric="1.2" dfric="1.0">
<control-input axis="/controls/flight/rudder" control="STEER" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="gear/gear[0]/steering-norm" />
<control-input axis="/controls/gear/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<gear x="-2.08669" y="5.50051" z="-5.663" compression="1.1" sfric="0.6" dfric="0.5"> <!-- Wing left main -->
<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-speed control="EXTEND" transition-time="10.0"/>
</gear>
<gear x="-5.16088" y="1.91819" z="-5.663" compression="1.1" sfric="0.6" dfric="0.5"> <!-- Body left main -->
<control-input control="STEER" axis="/controls/gear/main-gear-steering-norm" src0="-1.0" dst0="-0.191986214" src1="1.0" dst1="0.226892799" />
<control-output control="STEER" prop="gear/gear[2]/steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="10.0"/>
</gear>
<gear x="-5.16088" y="-1.91819" z="-5.663" compression="1.1" sfric="0.6" dfric="0.5"> <!-- Body right main -->
<control-input control="STEER" axis="/controls/gear/main-gear-steering-norm" src0="-1.0" dst0="-0.226892799" src1="1.0" dst1="0.191986214" />
<control-output control="STEER" prop="gear/gear[3]/steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="10.0"/>
</gear>
<gear x="-2.08669" y="-5.50051" z="-5.663" compression="1.1" sfric="0.6" dfric="0.5"> <!-- Wing right main -->
<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[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="10.0"/>
</gear>
<!-- Fuel Tanks -->
<!-- Maximum Fuel Capacity Intercontinental: 63,034 (59,734 without the rear stabilizer tanks) U.S. gallons (242,470 L) -->
<!-- 63034 * 6.84 = 431152.6 (- 3300 * 6.84)-->
<tank x="3.9" y="0" z="-1.45" jet="true" capacity="116489.8"/>
<tank x="1.5" y="8.0" z="-1.45" jet="true" capacity="107493.6"/>
<tank x="1.5" y="-8.0" z="-1.45" jet="true" capacity="107493.6"/>
<tank x="-4.0" y="12.1" z="-0.85" jet="true" capacity="29694.4"/>
<tank x="-4.0" y="-12.1" z="-0.85" jet="true" capacity="29694.4"/>
<tank x="-6.1" y="16.3" z="0.15" jet="true" capacity="8857.4"/>
<tank x="-6.1" y="-16.3" z="0.15" jet="true" capacity="8857.4"/>
<tank x="-33.95" y="0" z="3.58" jet="true" capacity="22572.0"/>
<!-- Crew Weight -->
<weight x="28.106" y="0.0" z="3.313" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="2.714" y="0" z="-1.4" mass-prop="/sim/weight[1]/weight-lb"/>
<!-- Pax/Cargo Weight -->
<ballast x="28.0" y="0" z="-3.4" mass="120000"/>
<ballast x="-5.0" y="0" z="-2.5" mass="120000"/>
</airplane>