Repository navigation
Expand file tree
/
Copy pathMD-11.xml
More file actions
171 lines (152 loc) · 9.88 KB
/
Copy pathMD-11.xml
File metadata and controls
171 lines (152 loc) · 9.88 KB
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
<?xml version="1.0" encoding="UTF-8" ?>
<airplane version="YASIM_VERSION_32" mass="283975">
<!-- Approach configuration based on stall chart http://tinypic.com/hsqd1l.jpg (from airliners.net thread http://www.airliners.net/aviation-forums/tech_ops/read.main/135496/) -->
<approach speed="152" aoa="4.3" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.3" />
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.3" />
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.3" />
<control-setting axis="/controls/flight/flaps" value="0.70" />
<control-setting axis="/controls/flight/slats" value="1.0" />
<control-setting axis="/controls/gear/gear-down" value="1.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="105000.0" />
</approach>
<!-- Cruise configuration -->
<cruise speed="493" alt="35000" fuel="0.8" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.75" />
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.75" />
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.75" />
<control-setting axis="/controls/flight/flaps" value="0.0" />
<control-setting axis="/controls/flight/slats" value="0.0" />
<control-setting axis="/controls/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="105000.0" />
</cruise>
<!-- <cockpit x="16.0" y="0.75" z="-0.8" />-->
<!-- Fuselage -->
<fuselage ax="17.74" ay="0.0" az="5.18" bx="-18.013" by="0.0" bz="5.133" width="6.0" taper="1.0" midpoint="1.0" />
<fuselage ax="27.67" ay="0.0" az="4.843" bx="17.74" by="0.0" bz="5.18" width="6.0" taper="0.14" midpoint="1.0" />
<fuselage ax="-18.013" ay="0.0" az="5.133" bx="-32.48" by="0.0" bz="6.101" width="6.0" taper="0.22" midpoint="0.0" />
<wing x="-1.08" y="3.0" z="4.235" length="28.06" chord="12.0" sweep="35.0" taper="0.31" camber="0.20" dihedral="6.4" incidence="3.2" twist="-2.9" idrag="1.7">
<stall aoa="8.6" width="5" peak="0.8" />
<flap0 start="0.0" end="0.52" lift="1.6" drag="2.1" />
<flap1 start="0.53" end="0.825" lift="1.2" drag="1.4" />
<slat start="0.0" end="0.85" aoa="3.0" drag="1.1" />
<spoiler start="0.03" end="0.45" lift="0.5" drag="1.6" />
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT" src0="0" dst0="0" src1="0.1428" dst1="1.0"/>
<control-output control="SLAT" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="78"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="SPOILER" transition-time="2"/>
<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>
<!-- Horizontal stabilizers -->
<hstab x="-27.341" y="0.91" z="5.632" length="11.5" chord="8.0" sweep="30.0" taper="0.4"
dihedral="10.6" camber="-0.1" twist="-1.0" idrag="1.1">
<stall aoa="15.0" width="7" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.5" 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 stabilizers -->
<vstab x="-25.7" y="0.0" z="7.68" length="12.0" chord="8.0" taper="0.4"
sweep="35.0" idrag="1.5">
<stall aoa="15" width="2" peak="1.5" />
<flap0 start="0.37" end="1.0" 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"/>
<control-speed control="FLAP0" transition-time="1.5" />
</vstab>
<!-- Engines -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="6.022" ay="8.138" az="2.536" bx="1.341" by="8.138" bz="2.536" width="2.742" taper="0.94" midpoint="0.0" />
<fuselage ax="6.022" ay="-8.138" az="2.536" bx="1.341" by="-8.138" bz="2.536" width="2.742" taper="0.94" midpoint="0.0" />
<fuselage ax="-22.427" ay="0.0" az="9.654" bx="-32.764" by="0.0" bz="9.293" width="2.84" taper="0.94" midpoint="0.0" />
<!-- Actual engines -->
<jet x="3.541" y="8.138" z="3.541" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1105.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[0]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="2.461" y="8.138" z="2.536" />
</jet>
<jet x="-30.564" y="0.0" z="10.5002" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1105.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[1]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-24.871" y="0.0" z="9.293" />
</jet>
<jet x="3.541" y="-8.138" z="3.541" mass="9047.0" thrust="61500.0" afterburner="0" rotate="0.0" n1-idle="33.0" n1-max="110.0" n2-idle="53.0" n2-max="103.0" tsfc="0.394" egt="700.0" epr="2.0" exhaust-speed="1105.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[2]/throttle-act" control="THROTTLE" />
<control-input axis="/controls/engines/engine[2]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[2]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="2.461" y="-8.138" z="2.536" />
</jet>
<!-- Pushback -->
<thruster x="20.6395" y="0.00" z="0.7" vx="1" vy="0" vz="0" thrust="12000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- Nosegear -->
<gear x="20.6395" y="0.0" z="0.7" compression="0.4" spring="0.8" damp="4.0">
<!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<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="15"/>
</gear>
<!-- Left main gears -->
<gear x="-4.7637" y="-5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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="19" />
</gear>
<!-- Right main gears -->
<gear x="-4.7637" y="5.3128" z="0.65" compression="0.7" spring="0.6" damp="1.0">
<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-speed control="EXTEND" transition-time="19" />
</gear>
<!-- Center gear -->
<gear x="-4.7637" y="0" z="0.5586" compression="0.7" spring="0.6" damp="1.0">
<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[3]/position-norm" />
<control-speed control="EXTEND" transition-time="15" />
</gear>
<!-- Fuel and payload -->
<!-- Left wing tanks-->
<tank x="-3.0" y="7.5" z="3.5" jet="true" capacity="40602" />
<!-- Center tank -->
<tank x="-1.08" y="0.0" z="3.0503" jet="true" capacity="64038" />
<!-- Right wing tanks -->
<tank x="-3.0" y="-7.5" z="3.5" jet="true" capacity="40602" />
<tank x="-1.08" y="0.0" z="3.0503" jet="true" capacity="98108" />
<tank x="-27.341" y="0" z="14.7597" jet="true" capacity="13400" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="25.0" y="0.0" z="2.3" mass="50000.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-8.8" y="0.0" z="2.3" mass="160000.0" />
<!-- Payload information from http://www.acp-logistics.com/DC-10-charter-mcdonnell-douglas.html -->
<!-- Crew -->
<weight x="25.0" y="0.0" z="4.0" mass-prop="/sim/weight[0]/weight-lb" />
<!-- PAX/Cargo -->
<weight x="-2.75" y="0.0" z="3.2" mass-prop="/sim/weight[1]/weight-lb" />
</airplane>