forked from dogsaysmoo/ATR-72-500
/
ATR-72-500.xml
191 lines (166 loc) · 8.48 KB
/
ATR-72-500.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
<?xml version="1.0" encoding="UTF-8" ?>
<!--
ATR 72-500 for FlightGear YASim FDM
By Ryan M
Specifications can be viewed on Airliners.net:
http://www.airliners.net/aircraft-data/stats.main?id=42
And Wikipedia (of course ;) ):
http://en.wikipedia.org/wiki/ATR_72#Specifications_.28ATR_72.E2.80.93500.29
-->
<airplane mass="28550">
<approach speed="90" aoa="7.0" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.6" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.6" />
<control-setting axis="/controls/engines/engine[0]/condition-lever" value="1.0" />
<control-setting axis="/controls/engines/engine[1]/condition-lever" value="1.0" />
<control-setting axis="/systems/hydraulics/blue/flight/flaps" value="1.0" />
<control-setting axis="/systems/hydraulics/green/gear/gear-down" value="1.0" />
<solve-weight idx="0" weight="600" />
<solve-weight idx="1" weight="8829" />
<solve-weight idx="2" weight="0" />
<!--solve-weight idx="1" weight="6259" /-->
</approach>
<!-- Service ceiling is actually 25000 ft -->
<cruise speed="276" alt="20000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.9" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.9" />
<control-setting axis="/controls/engines/engine[0]/condition-lever" value="1.0" />
<control-setting axis="/controls/engines/engine[1]/condition-lever" value="1.0" />
<control-setting axis="/systems/hydraulics/blue/flight/flaps" value="0.0" />
<control-setting axis="/systems/hydraulics/green/gear/gear-down" value="0.0" />
<solve-weight idx="0" weight="600" />
<solve-weight idx="1" weight="8829" />
<solve-weight idx="2" weight="0" />
<!--solve-weight idx="1" weight="6259" /-->
</cruise>
<cockpit x="11.0" y="0.6" z="-1.0" />
<!-- FUSELAGE -->
<!-- Main fuselage -->
<fuselage ax="10.363" ay="0.0" az="-1.73" bx="-5.05" by="0.0" bz="-1.73" width="2.7" taper="1.0" midpoint="1.0" />
<!-- Nose cone -->
<fuselage ax="13.581" ay="0.0" az="-2.118" bx="10.363" by="0.0" bz="-1.73" width="2.7" taper="0.0" midpoint="1.0" />
<!-- Rear cone -->
<fuselage ax="-5.05" ay="0.0" az="-1.73" bx="-13.585" by="0.0" bz="-1.155" width="2.7" taper="0.184" midpoint="0.0" />
<!-- WINGS -->
<wing x="1.12" y="0.0" z="-0.24" length="13.524" chord="2.5" sweep="0.0" taper="0.57" camber="0.1" incidence="3.0" twist="-1.0" idrag="2.0">
<stall aoa="15.0" width="5.0" peak="0.8" />
<flap0 start="0.086" end="0.707" lift="1.5" drag="2.0" />
<flap1 start="0.707" end="0.98" lift="1.2" drag="1.5" />
<spoiler start="0.11" end="0.7" lift="0.0" drag="1.0" />
<control-input axis="/systems/hydraulics/blue/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-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="10.0" />
<control-speed control="FLAP1" transition-time="1.5" />
</wing>
<!-- ELEVATORS -->
<hstab x="-12.07" y="0.0" z="2.93" length="3.36" chord="1.92" sweep="4.0" taper="0.63" camber="0.01" twist="-1.0" idrag="2.0">
<stall aoa="15.0" width="5.0" peak="0.8" />
<flap0 start="0.0" end="0.969" lift="1.5" 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>
<!-- TAIL -->
<vstab x="-8.39" y="0.0" z="-0.87" length="6.17" chord="7.68" sweep="41.393" taper="0.24">
<stall aoa="15.0" width="5.0" peak="0.8" />
<flap0 start="0.0" end="0.85" lift="1.2" 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>
<!-- ENGINES -->
<propeller
x="2.327"
y="3.86"
z="-0.61"
mass="396.8"
moment="27.928"
radius="1.965"
cruise-power="2100"
cruise-speed="280"
cruise-rpm="1200.0"
cruise-alt="20000.0"
min-rpm="900.0" max-rpm="1300.0">
<turbine-engine
eng-power="2750" eng-rpm="1300" alt="15000"
flat-rating="2475" min-n2="70" max-n2="100" bsfc="0.459"/>
<actionpt x="4.827" y="3.86" z="-0.61" />
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/condition-lever" control="CONDLEVER" />
</propeller>
<propeller
x="2.327"
y="-3.86"
z="-0.61"
mass="396.8"
moment="-27.928"
radius="1.965"
cruise-power="2100"
cruise-speed="280"
cruise-rpm="1200.0"
cruise-alt="20000.0"
min-rpm="900.0" max-rpm="1300.0">
<turbine-engine
eng-power="2750" eng-rpm="1300" alt="15000"
flat-rating="2475" min-n2="70" max-n2="100" bsfc="0.459"/>
<actionpt x="4.827" y="-3.86" z="-0.61" />
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/condition-lever" control="CONDLEVER" />
</propeller>
<!-- Reverse thrusters (YASim does not have reverse thrust for turboprops, so thrusters are used instead) -->
<thruster x="4.827" y="3.86" z="-3.747" vx="-1" vy="0" vz="0" thrust="3000">
<control-input axis="/controls/engines/engine[0]/reverser-cmd-norm" control="THROTTLE" src0="0" dst0="0" src1="1" dst1="1" />
</thruster>
<thruster x="4.827" y="-3.86" z="-3.747" vx="-1" vy="0" vz="0" thrust="3000">
<control-input axis="/controls/engines/engine[1]/reverser-cmd-norm" control="THROTTLE" src0="0" dst0="0" src1="1" dst1="1" />
</thruster>
<!-- LANDING GEARS -->
<!-- Pushback -->
<thruster x="11.837" y="0.0" z="-3.747" vx="1" vy="0" vz="0" thrust="9000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" dst0="-1" src1="1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="11.837" y="0.0" z="-3.747" compression="0.3" sfric="0.7" dfric="0.5">
<control-input axis="/controls/gear/steering-deg" control="STEER" src0="-60" dst0="-1" src1="60" dst1="1" />
<control-input axis="/systems/hydraulics/green/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="10.0" />
</gear>
<!-- Left main gear -->
<gear x="0.88" y="1.922" z="-3.859" compression="0.4" sfric="0.7" dfric="0.5">
<control-input axis="/systems/hydraulics/green/gear/brake-left" control="BRAKE" />
<control-input axis="/systems/hydraulics/blue/gear/brake-parking" control="BRAKE" />
<control-input axis="/systems/hydraulics/green/gear/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<!-- Right main gear -->
<gear x="0.88" y="-1.922" z="-3.859" compression="0.4" sfric="0.7" dfric="0.5">
<control-input axis="/systems/hydraulics/green/gear/brake-right" control="BRAKE" />
<control-input axis="/systems/hydraulics/blue/gear/brake-parking" control="BRAKE" />
<control-input axis="/systems/hydraulics/green/gear/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm" />
<control-speed control="EXTEND" transition-time="10.0" />
</gear>
<!-- FUEL AND PAYLOAD -->
<!-- Total fuel capacity: 11,025 pounds -->
<!-- Left wing fuel tank -->
<tank x="1.1" y="5.0" z="-0.2" jet="true" capacity="5512.0" />
<!-- Right wing fuel tank -->
<tank x="1.1" y="-5.0" z="-0.2" jet="true" capacity="5512.0" />
<!-- Ferry Tank -->
<!--tank x="1.0" y="0.0" z="-1.5" jet="true" capacity="3212.0" /-->
<!-- Crew -->
<weight x="11.0" y="0.0" z="-1.5" mass-prop="/sim/weight[0]/weight-lb" idx="0" />
<!-- PAX/Cargo -->
<weight x="1.0" y="0.0" z="-1.5" mass-prop="/sim/weight[1]/weight-lb" idx="1" />
<!-- Extra Fuel tanks for ferry ops -->
<weight x="1.0" y="0.0" z="-1.5" mass-prop="/sim/weight[2]/weight-lb" idx="1" />
<!-- Ballast to adjust center of gravity -->
<ballast x="10.0" y="0.0" z="-2.0" mass="10000.0" />
</airplane>