forked from YoRyan/FlightGear-CRJ700-family
-
Notifications
You must be signed in to change notification settings - Fork 6
/
Copy pathCRJ900.xml
216 lines (198 loc) · 11.8 KB
/
CRJ900.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
<?xml version="1.0" encoding="UTF-8" ?>
<!--
Bombardier CRJ900 YASim FDM
By Ryan Miller
Specifications can be viewed on Boeing's website:
http://www.crj.bombardier.com/CRJ/en/specifications.jsp?langId=en&crjId=900
More can be found on Wikipedia:
http://en.wikipedia.org/wiki/Bombardier_CRJ700_series#Specifications
<weight n="1">
<name>PAX</name>
<max-lb>15165</max-lb>
</weight>
<weight n="2">
<name>Main Cargo</name>
<max-lb>4375</max-lb>
</weight>
<weight n="3">
<name>Aft Cargo</name>
<max-lb>1700</max-lb>
</weight>
-->
<airplane mass="47250" mlw-lbs="73500" mtow-lbs="80500" cg-min="0.11" cg-max="0.32" version="2018.1">
<!-- Approach speed is 125-140 knots http://forums.jetcareers.com/airline-pilots/57253-crj-900-v-speeds.html#post758173 -->
<approach speed="125" aoa="2.0" 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/flight/flaps-cmd" value="1.0" />
<control-setting axis="/controls/flight/slats-cmd" value="1.0" />
<control-setting axis="/fcs/gear-down" value="1.0" />
<solve-weight idx="0" weight="380.0" />
<solve-weight idx="1" weight="5000.0" />
<solve-weight idx="2" weight="1500.0" />
<solve-weight idx="3" weight="750.0" />
</approach>
<cruise speed="560" alt="40000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.85" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.85" />
<control-setting axis="/controls/flight/flaps-cmd" value="0.0" />
<control-setting axis="/controls/flight/slats-cmd" value="0.0" />
<control-setting axis="/fcs/gear-down" value="0.0" />
<solve-weight idx="0" weight="380.0" />
<solve-weight idx="1" weight="12000.0" />
<solve-weight idx="2" weight="3400.0" />
<solve-weight idx="3" weight="1600.0" />
</cruise>
<cockpit x="15.045" y="0.528" z="-0.468" />
<!-- Fuselage -->
<fuselage ax="14.122" ay="0.0" az="-1.043" bx="-7.01" by="0.0" bz="-1.043" width="2.78" taper="1.0" midpoint="1.0" />
<fuselage ax="18.193" ay="0.0" az="-1.733" bx="14.122" by="0.0" bz="-1.043" width="2.78" taper="0.1" midpoint="1.0" />
<fuselage ax="-7.01" ay="0.0" az="-1.043" bx="-15.608" by="0.0" bz="-0.696" width="2.78" taper="0.22" midpoint="0.0" />
<!-- Wings -->
<!-- Inner segment -->
<wing x="0.08" y="1.226" z="-2.034" length="3.7" chord="5.085" sweep="17.5" taper="0.63"
dihedral="1.5" incidence="5.0" twist="-2.0"
camber="0.05"
flow="TRANSONIC">
<stall aoa="10.0" width="4" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.39" drag="1.99" />
<slat start="0.22" end="1.0" aoa="3.0" drag="1.1" />
<spoiler start="0.18" end="1.0" lift="0.6" drag="2.5" />
<control-input axis="/controls/flight/flaps-cmd" control="FLAP0" />
<control-input axis="/controls/flight/slats-cmd" control="SLAT" />
<control-input axis="/surface-positions/spoiler-ground-pos-norm" control="SPOILER" />
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm" />
<control-output control="SLAT" prop="/surface-positions/slat-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-inner-pos-norm" />
<control-speed control="FLAP0" transition-time="16.72" />
<control-speed control="SLAT" transition-time="8.9" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!-- Outer segment -->
<wing append="1" length="7.2" sweep="24.0" taper="0.4" dihedral="3.0" twist="-2.9"
camber="0.01"
flow="TRANSONIC">
<stall aoa="7.0" width="3" peak="1.2" />
<flap0 start="0.0" end="0.51" lift="1.4" drag="2.5" />
<flap1 start="0.51" end="0.8" lift="1.35" drag="1.25" />
<slat start="0.0" end="1.0" aoa="3.0" drag="1.1" />
<spoiler start="0.0" end="0.31" lift="0.6" drag="2.5" />
<control-input axis="/controls/flight/flaps-cmd" control="FLAP0" />
<control-input axis="/fcs/aileron-hydraulic-cmd-norm" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/slats-cmd" control="SLAT" />
<control-input axis="/surface-positions/left-ob-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="left" control="SPOILER" />
<control-input axis="/surface-positions/left-ib-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="left" control="SPOILER" />
<control-input axis="/surface-positions/right-ob-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="right" control="SPOILER" />
<control-input axis="/surface-positions/right-ib-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="right" control="SPOILER" />
<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-output control="SLAT" prop="/surface-positions/slat-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-outer-pos-norm" />
<control-speed control="FLAP0" transition-time="16.72" />
<control-speed control="FLAP1" transition-time="2.0" />
<control-speed control="SLAT" transition-time="8.9" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!-- Horizontal stabilizers -->
<hstab x="-15.62" y="0.149" z="2.851" length="4.6" chord="2.574" sweep="26.0" taper="0.4" dihedral="-5.2"
camber="0"
twist="-1.0"
incidence-min-deg="-13"
incidence-max-deg="2"
incidence="5.0">
<stall aoa="15.0" width="7" peak="1.5" />
<flap0 start="0.0" end="0.82" lift="1.45" drag="1.4" />
<control-input axis="/fcs/elevator-cmd-norm" control="FLAP0" />
<control-input axis="/controls/flight/elevator-trim" control="FLAP0" />
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm" />
<control-speed control="FLAP0" transition-time="1.5" />
<control-input axis="/controls/flight/hstab-trim" control="INCIDENCE" />
<control-speed control="INCIDENCE" transition-time="20" />
<control-output control="INCIDENCE" prop="/surface-positions/hstab-yasim-rad" />
</hstab>
<!-- Vertical stabilizers -->
<vstab x="-13.305" y="0.0" z="-0.158" length="4.2" chord="3.498" taper="0.7" sweep="36.0" idrag="1.0">
<stall aoa="15" width="2" peak="1.5" />
<flap0 start="0.0" end="0.72" lift="1.5" drag="1.4" />
<control-input axis="/fcs/rudder-cmd-norm" 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" />
<control-speed control="FLAP0" transition-time="1.5" />
</vstab>
<!-- Engines -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="-7.667" ay="2.27" az="-0.264" bx="-9.816" by="2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<fuselage ax="-7.667" ay="-2.27" az="-0.264" bx="-9.816" by="-2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<!-- GE CF34-8C5 -->
<jet x="-8.925" y="2.27" z="-0.319" mass="2450.0" afterburner="0" rotate="-2.5"
thrust="14510"
n1-idle="21.0" n1-max="99.5" n2-idle="59.0" n2-max="99.4"
tsfc="0.68" egt="1000.0" epr="28.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE" src0="0" src1="1" dst0="0.0391" dst1="1" />
<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="-10.983" y="2.27" z="-0.409" />
</jet>
<jet x="-8.925" y="-2.27" z="-0.319" mass="2450.0" afterburner="0" rotate="-2.5"
thrust="14510"
n1-idle="21.0" n1-max="99.5" n2-idle="59.0" n2-max="99.4"
tsfc="0.68" egt="1000.0" epr="28.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" src0="0" src1="1" dst0="0.0391" dst1="1" />
<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="-10.983" y="-2.27" z="-0.409" />
</jet>
<!-- Landing gear -->
<!-- Pushback -->
<thruster x="16.172" y="0.0" z="-3.459" vx="1" vy="0" vz="0" thrust="10000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" dst0="-1" src1="1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="16.172" y="0.0" z="-3.459" compression="0.4" spring="0.7" damp="4.0">
<control-input axis="/fcs/nose-gear-steer-deg" control="STEER" src0="-80" dst0="-1" src1="80" dst1="1" />
<control-input axis="/fcs/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="9.2" />
</gear>
<!-- Left main gear -->
<gear x="-1.356" y="2.054" z="-3.81" compression="0.35" spring="0.6" damp="1.0">
<control-input axis="/fcs/brake-left-cmd-norm" control="BRAKE" />
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/fcs/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm" />
<control-speed control="EXTEND" transition-time="9.2" />
</gear>
<!-- Right main gear -->
<gear x="-1.356" y="-2.054" z="-3.81" compression="0.35" spring="0.6" damp="1.0">
<control-input axis="/fcs/brake-right-cmd-norm" control="BRAKE" />
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/fcs/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm" />
<control-speed control="EXTEND" transition-time="9.2" />
</gear>
<!-- Fuel and payload -->
<!-- Left wing tank -->
<tank x="-1.37" y="5.22" z="-1.9" jet="true" capacity="7554" />
<!-- Right wing tank -->
<tank x="-1.37" y="-5.22" z="-1.9" jet="true" capacity="7554" />
<!-- Center tank -->
<tank x="0.155" y="0.0" z="-2.2" jet="true" capacity="4642" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="15.3" y="0.0" z="-1.9" mass="3100.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-1.29" y="0.0" z="-2.6" mass="5000.0" />
<!-- Crew -->
<weight x="14.94" y="0.0" z="-1.0" mass-prop="/sim/weight[0]/weight-lb" solve-weight="1" idx="0" />
<!-- PAX -->
<weight x="1.0" y="0.0" z="-1.0" mass-prop="/sim/weight[1]/weight-lb" solve-weight="1" idx="1" />
<!-- Main Cargo -->
<weight x="6.6" y="0.0" z="-2.1" mass-prop="/sim/weight[2]/weight-lb" solve-weight="1" idx="2" />
<!-- Aft Cargo -->
<weight x="-8.8" y="0.0" z="-1.5" mass-prop="/sim/weight[3]/weight-lb" solve-weight="1" idx="3" />
</airplane>