Fix of LOC/GS scale flickering when LOC/GS capture.
[fg:toms-fgdata.git] / Aircraft / 777 / 777-300.xml
1 <!--\r
2 \r
3 Boeing 777-300 YASim\r
4 =======================\r
5 \r
6 The Boeing 777-300 is a stretched version of the 777, powered by the most powerful turbofan engines, seating 328 to 394 passengers in a typical three class seating arrangement or 550 passengers in a single economy class arrangement.\r
7 This aircraft is the latest derivative of the 777 family and the first airplane was given to Cathay Pacific in May 1998. 60 aircraft were sent and production is complete.\r
8 The stretched 777-300 is designed as a substitute for early generation 747s (747-100s and 200s). Compared to the older 747s the stretched 777 has similar passenger capacity and range, but burns one third less fuel and present 40% lower maintenance costs.\r
9 \r
10 Specs:\r
11 \r
12 777-300 - Either \r
13 2 400kN (90,000lb) Pratt and Whitney PW-4090 turbofans, or \r
14 2 436kN (98,000lb) PW-4098s, or \r
15 2 409kN (92,000lb) Rolls-Royce Trent 892s, or \r
16 2 409kN (93,700lb) General Electric GE90-94B.\r
17 \r
18 Typical Cruise = 0.84 Mach / 35000 ft\r
19 Max Speed = 0.87 / 35000 ft\r
20 \r
21 777-300 - Typical cruising speed 893km/h (482kt). Range with 386 three class passengers 10,595km (5720nm).\r
22 777-300ER - Range with 365 passengers 13,427km (7,250nm).\r
23 \r
24 Wing span: 60.93m\r
25 Length: 63.73 m\r
26 Tail Height: 18.51m\r
27 Diameter : 6.19 m\r
28 Wing Area: 427.8m2\r
29 Max Fuel :45,220 US gal\r
30 Max TO weight: 660,000 lbs\r
31 Max Landing weight: 524,000 lbs\r
32 \r
33 TO speed : 145 kt\r
34 Landing speed : 131 kt\r
35 \r
36 Leading edge MAC = -3.132\r
37 \r
38 Vr 137\r
39 V2 147\r
40 \r
41 Datum 92.5 in forward of nose - 2.3495 m\r
42 MAC 278.51 in - 7.074154 m\r
43 \r
44 References : \r
45 \r
46 http://www.airliners.net/aircraft-data/stats.main?id=107\r
47 http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/0ba575940677fa2d8525670c00685612/$FILE/E00049en.PDF\r
48 http://www.boeing.com/commercial/airports/faqs/arcandapproachspeeds.pdf\r
49 \r
50 -->\r
51 <airplane mass="353600">\r
52 \r
53 <!-- Approach configuration \r
54  Reference : \r
55  \r
56  Airport Reference Code and Approach Speeds for Boeings Airplanes\r
57  http://www.boeing.com/commercial/airports/faqs/arcandapproachspeeds.pdf\r
58  \r
59  772ER FG default + reference difference.\r
60 -->\r
61 <approach speed="145" aoa="3" fuel="0.2">\r
62     <control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.25"/>\r
63     <control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.25"/>\r
64     <control-setting axis="/controls/flight/flaps" value="1"/>\r
65     <control-setting axis="/surface-positions/slats" value="1"/>\r
66     <control-setting axis="/controls/gear/gear-down" value="1"/>\r
67     <solve-weight idx="0" weight="350"/>\r
68     <solve-weight idx="1" weight="45000"/>\r
69 </approach>\r
70 \r
71 <!-- Cruise configuration -->\r
72 <cruise speed="490" alt="38000" fuel="0.8">\r
73     <control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.95"/>\r
74     <control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.95"/>\r
75     <control-setting axis="/controls/flight/flaps" value="0.0"/>\r
76     <control-setting axis="/controls/flight/elevator-trim" value="0"/>\r
77     <control-setting axis="/controls/gear/gear-down" value="0"/>\r
78     <solve-weight idx="0" weight="350"/>\r
79     <solve-weight idx="1" weight="45000"/>\r
80 </cruise>\r
81 \r
82 <!-- Cockpit position -->\r
83 <cockpit x="28.0381" y="0.5" z="0.75"/>\r
84 \r
85 <!-- Fuselage -->\r
86 <fuselage ax="30.5981" ay="0" az="-0.64" bx="21.4691" by="0.00" bz="0.0"\r
87     width="6.2" taper="0.0" midpoint="1.0"/>\r
88 <fuselage ax="21.4691" ay="0" az="0" bx="-24.7003" by="0.00" bz="0.0"\r
89     width="6.2" taper="1.0" midpoint="0.5"/>\r
90 <fuselage ax="-24.7003" ay="0" az="0" bx="-41.7003" by="0.00" bz="1.2"\r
91     width="6.2" taper="0.0" midpoint="0.0"/>\r
92 \r
93 <!-- Engines body -->\r
94 <fuselage ax="4.0" ay="9.8" az="-3" bx="-1.8" by="9.8" bz="-3"\r
95     width="3.8" taper="1.0"/>\r
96 <fuselage ax="4.0" ay="-9.8" az="-3" bx="-1.8" by="-9.8" bz="-3"\r
97     width="3.8" taper="1.0"/>\r
98 \r
99 <!-- Wings -->\r
100   <wing x="-0.0" y="3.095" z="-1.66" length="30.6" chord="10.0" sweep="28.7"\r
101         taper="0.15" dihedral="7" camber="0.01" incidence="2" twist="-2">\r
102       <stall aoa="16" width="6" peak="1.5"/>\r
103       <flap0 start="0" end=".56" lift="1.5" drag="1.7"/>\r
104       <flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>\r
105       <slat start="0" end="1" aoa="2" drag="1"/>\r
106       <spoiler start="0.2" end="0.6" lift="0.2" drag="2.0"/>\r
107       <control-input axis="/controls/flight/flaps" control="FLAP0"/>\r
108       <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>\r
109       <control-input axis="/surface-positions/flap-pos-norm" control="SLAT"\r
110                      src0="0" dst0="0" src1="0.1428" dst1="1.0"/>\r
111       <control-output control="SLAT" prop="/surface-positions/slats"/>\r
112       <control-speed control="FLAP0" transition-time="78"/>\r
113       <control-input axis="/controls/flight/speedbrake" control="SPOILER"/>\r
114       <control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>\r
115       <control-speed control="SPOILER" transition-time="2"/>\r
116       <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>\r
117       <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>\r
118       <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>\r
119       <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>\r
120   </wing>\r
121 \r
122   <hstab x="-31.0" y="1.5" z="1.0" chord="6.0" length="10.84" taper=".20"\r
123          sweep="28" dihedral="7" camber="0.0">\r
124     <stall aoa="18" width="5" peak="1.5"/>\r
125     <flap0 start="0" end="1" lift="1.4" drag="1.2"/>\r
126   <control-input axis="/controls/flight/elevator" control="FLAP0"/>\r
127   <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>\r
128   <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>\r
129 </hstab>\r
130 \r
131   <vstab x="-30.0" y="0.00" z="2.7" chord="8.0" length="12.2" taper="0.3"\r
132          sweep="33">\r
133   <stall aoa="14" width="5" peak="1.5"/>\r
134     <flap0 start="0" end="1" lift="1.4" drag="1.2"/>\r
135   <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>\r
136   <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>\r
137   <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"\r
138           min="1" max="-1"/>\r
139 </vstab>\r
140 \r
141 <!-- General Electric GE90-94B \r
142 \r
143 GEN ELEC-GE 90-94B Thrust=93700 lb Mass=16644 lb Cruise SFC 0.545 (lb/hr/lb) ??\r
144 -->\r
145 <jet x="1.16" y="9.89"  z="-2.995" mass="16644" thrust="93700" spool-time="3"\r
146 egt="825" tsfc="0.30" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="117" reverse="0.4">\r
147   <control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE"/>\r
148   <control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>\r
149     <control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>\r
150     <control-speed control="REVERSE_THRUST" transition-time="4"/>\r
151 <actionpt x="-2.7" y="9.89" z="-2.995"/>\r
152 </jet>\r
153 \r
154 <jet x="1.16" y="-9.89"  z="-2.995" mass="16644" thrust="93700" spool-time="3"\r
155 egt="825" tsfc="0.30" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="117" reverse="0.4">\r
156   <control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE"/>\r
157   <control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>\r
158     <control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>\r
159     <control-speed control="REVERSE_THRUST" transition-time="4"/>\r
160 <actionpt x="-2.7" y="-9.89" z="-2.995"/>\r
161 </jet>\r
162 \r
163   <!-- nose -->\r
164   <gear x="19.28"  y="0.00" z="-5.55"\r
165         compression="0.7" spring="1.2" damp="1" sfric="1.5" dfric="1.0">\r
166     <!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->\r
167     <control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />\r
168     <control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />\r
169     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>\r
170     <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>\r
171     <control-speed control="EXTEND" transition-time="19"/>\r
172   </gear>\r
173 \r
174   <gear x="-6.39" y="5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">\r
175     <control-input axis="/autopilot/autobrake/left-brake-output" control="BRAKE"/>\r
176     <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>\r
177     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>\r
178     <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>\r
179     <control-speed control="EXTEND" transition-time="20"/>\r
180   </gear>\r
181 \r
182   <gear x="-6.39" y="-5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">\r
183     <control-input axis="/autopilot/autobrake/right-brake-output" control="BRAKE"/>\r
184     <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>\r
185     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>\r
186     <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>\r
187     <control-speed control="EXTEND" transition-time="20"/>\r
188   </gear>\r
189 \r
190   <!-- aft axle on left main gear -->\r
191   <gear x="-7.8" y="5.6" z="-6.22" compression="3.0" spring="1.2" >\r
192     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>\r
193     <control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>\r
194     <control-speed control="EXTEND" transition-time="20"/>\r
195     <!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->\r
196     <control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />\r
197     <control-output control="STEER" prop="/controls/gear/maingear-l-steering-angle-rad" />\r
198   </gear>\r
199 \r
200   <!-- aft axle on right main gear -->\r
201   <gear x="-7.8" y="-5.6" z="-6.22" compression="3.0" spring="1.2">\r
202     <control-input axis="/controls/gear/gear-down" control="EXTEND"/>\r
203     <control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>\r
204     <control-speed control="EXTEND" transition-time="20"/>\r
205     <!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->\r
206     <control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />\r
207     <control-output control="STEER" prop="/controls/gear/maingear-r-steering-angle-rad" />\r
208   </gear>\r
209 \r
210   <!--  fake gear as tail contact point for tailstrikes -->\r
211   <gear x="-19.84"  y="0.00" z="-3.38"\r
212         compression="0.1" spring="1" damp="1" sfric="0.5" dfric="0.5">\r
213   </gear>\r
214 \r
215   <tank x="-4.3" y="5" z="-1.5" jet="true" capacity="64100"/>\r
216   <tank x="-4.3" y="0" z="-2.5" jet="true" capacity="174900"/>\r
217   <tank x="-4.3" y="-5" z="-1.5" jet="true" capacity="64100"/>\r
218 \r
219 <weight x="27.2381" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>\r
220 <weight x="-9.0003" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>\r
221 \r
222   <ballast x="-34.7003" y="0" z="4" mass="-70000"/>\r
223 \r
224 <thruster x="24.5181"  y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">\r
225   <control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE"\r
226   src0="-1" src1="1" dst0="-1" dst1="1"/>\r
227   </thruster>\r
228 \r
229 </airplane>\r