Adjust the locations of the engines, tanks, CG, Eyepoint, add different pointmasses...
[fg:toms-fgdata.git] / Aircraft / fokker100 / fokker100.xml
1 <FDM_CONFIG NAME="Fokker 100" VERSION="1.65" RELEASE="ALPHA">
2 <!--
3   File:     Fokker 100.xml
4   Author:   Aero-Matic v 0.71
5
6   Sources:
7      *  Butterworth-Heinemann - Civil Jet Aircraft Design (BH)
8         http://www.bh.com/companions/034074152X/appendices/data-a/default.htm
9      *  Lissys - PIANO aircraft analysis software 
10         http://www.lissys.demon.co.uk/f7tx2.html
11      *  Advanced Topics in Aerodynamics, Aerodynamic Database (AD)
12         http://aerodyn.org/HighLift/tables.html
13
14   Inputs:
15     name:          Fokker 100
16     type:          two-engine transonic transport
17     max weight:    95013.45 lb
18     wing span:     92.13048 ft
19     length:        115.32715 ft
20     wing area:     1006.5275 sq-ft
21     gear type:     tricycle
22     retractable?:  yes
23     # engines:     2
24     engine type:   turbine
25     engine layout: middle fuselage
26     yaw damper?    yes
27
28   Outputs:
29     wing loading:  94.40 lb/sq-ft
30     CL-alpha:      4.4 per radian
31     CL-0:          0.2
32     CL-max:        1.2
33     CD-0:          0.02
34     K:             0.043
35
36 -->
37
38  <METRICS>
39    AC_WINGAREA  1006.53
40    AC_WINGSPAN  92.13
41    AC_CHORD     12.41                   <!-- Lissys -->
42    AC_HTAILAREA 244.47                  <!-- Lissys -->
43    AC_HTAILARM  47.22                   <!-- Lissys -->
44    AC_VTAILAREA 178.83                  <!-- Lissys -->
45    AC_LV        37.62                   <!-- Lissys -->
46    AC_IXX       587012
47    AC_IYY       2125156
48    AC_IZZ       2519272
49    AC_IXZ       0
50    AC_EMPTYWT   54218                   <!-- BH -->
51    AC_CGLOC     587.4  0.0 -16.5
52    AC_AERORP    587.4  0.0 18.1
53    AC_EYEPTLOC  94.5 -22.4 49.2
54    AC_VRP       0 0 0
55
56    <!-- pilot -->
57    AC_POINTMASS  230.0 94.5  -22.4 25.6
58    <!-- co-pilot -->
59    AC_POINTMASS  230.0 94.5 22.4 25.6
60    <!-- 2 stuward(esse)s -->
61    AC_POINTMASS  400.0 206.0 22.4 25.6
62  </METRICS>
63  <UNDERCARRIAGE>
64   AC_GEAR NOSE_LG   137.0  0.0 -81.5 28504.0 9501.3  0.5  0.8  0.02 STEERABLE NONE  5.0 RETRACT
65   AC_GEAR LEFT_MLG  700.4 -113.0 -89.8 95013.4 19002.7  0.5  0.8  0.02 FIXED LEFT  0 RETRACT
66   AC_GEAR RIGHT_MLG 700.4 113.0 -89.8 95013.4 19002.7  0.5  0.8  0.02 FIXED RIGHT 0 RETRACT
67  </UNDERCARRIAGE>
68  <PROPULSION>
69   <AC_ENGINE FILE="Tay-651">
70     XLOC 1028.74
71     YLOC -101.6
72     ZLOC -49.2
73     PITCH 0
74     YAW 0
75     FEED 0
76     <AC_THRUSTER FILE="direct">
77       XLOC 1028.74
78       YLOC -101.6
79       ZLOC -49.2
80       PITCH 0
81       YAW 0
82     </AC_THRUSTER>
83   </AC_ENGINE>
84   <AC_ENGINE FILE="Tay-651">
85     XLOC 1028.74
86     YLOC 101.6
87     ZLOC -49.2
88     PITCH 0
89     YAW 0
90     FEED 1
91     <AC_THRUSTER FILE="direct">
92       XLOC 1028.74
93       YLOC 101.6
94       ZLOC -49.2
95       PITCH 0
96       YAW 0
97     </AC_THRUSTER>
98   </AC_ENGINE>
99   <AC_TANK TYPE="FUEL" NUMBER="0">
100     XLOC 587.4
101     YLOC 0
102     ZLOC -16.5
103     RADIUS 1 
104     CAPACITY  1377.0
105     CONTENTS   688.5
106   </AC_TANK>
107   <AC_TANK TYPE="FUEL" NUMBER="1">
108     XLOC 587.4
109     YLOC 0 
110     ZLOC -16.5
111     RADIUS 1 
112     CAPACITY  1377.0
113     CONTENTS   688.5
114   </AC_TANK>
115   <AC_TANK TYPE="FUEL" NUMBER="2">
116     XLOC 587.4
117     YLOC 0 
118     ZLOC -16.5
119     RADIUS 1 
120     CAPACITY  1377.0
121     CONTENTS   688.5
122   </AC_TANK>
123  </PROPULSION>
124  <FLIGHT_CONTROL NAME="Fokker 100">
125    <COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
126       INPUT   fcs/elevator-cmd-norm
127       INPUT   fcs/pitch-trim-cmd-norm
128       CLIPTO  -1 1
129    </COMPONENT>
130    <COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
131       INPUT   fcs/pitch-trim-sum
132       MIN     -0.350
133       MAX      0.300
134       OUTPUT  fcs/elevator-pos-rad
135    </COMPONENT>
136    <COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
137       INPUT   fcs/aileron-cmd-norm
138       INPUT   fcs/roll-trim-cmd-norm
139       CLIPTO  -1 1
140    </COMPONENT>
141    <COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
142       INPUT   fcs/roll-trim-sum
143       MIN    -0.35
144       MAX     0.35
145       OUTPUT  fcs/left-aileron-pos-rad
146    </COMPONENT>
147    <COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
148       INPUT  -fcs/roll-trim-sum
149       MIN    -0.35
150       MAX     0.35
151       OUTPUT  fcs/right-aileron-pos-rad
152    </COMPONENT>
153    <COMPONENT NAME="Rudder Command Sum" TYPE="SUMMER">
154       INPUT   fcs/rudder-cmd-norm
155       INPUT   fcs/yaw-trim-cmd-norm
156       CLIPTO  -1 1
157    </COMPONENT>
158    <COMPONENT NAME="Yaw Damper Rate" TYPE="SCHEDULED_GAIN">
159       INPUT        velocities/r-aero-rad_sec
160       SCHEDULED_BY aero/qbar-psf
161       ROWS         2
162        3.00        0.00
163       11.00        2.00
164    </COMPONENT>
165    <COMPONENT NAME="Yaw Damper Beta" TYPE="SCHEDULED_GAIN">
166       INPUT        aero/beta-rad
167       SCHEDULED_BY aero/qbar-psf
168       ROWS         2
169        3.00        0.00
170       11.00        0.00
171    </COMPONENT>
172    <COMPONENT NAME="Yaw Damper Sum" TYPE="SUMMER">
173       INPUT        fcs/yaw-damper-beta
174       INPUT        fcs/yaw-damper-rate
175       CLIPTO      -0.2 0.2
176    </COMPONENT>
177    <COMPONENT NAME="Yaw Damper Final" TYPE="SCHEDULED_GAIN">
178       INPUT        fcs/yaw-damper-sum
179       SCHEDULED_BY aero/qbar-psf
180       ROWS         2
181       2.99         0.0
182       3.00         1.0
183    </COMPONENT>
184    <COMPONENT NAME="Rudder Sum" TYPE="SUMMER">
185       INPUT   fcs/rudder-command-sum
186       INPUT   fcs/yaw-damper-final
187       CLIPTO  -1 1
188    </COMPONENT>
189    <COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
190       INPUT   fcs/rudder-sum
191       MIN     -0.35
192       MAX      0.35
193       OUTPUT  fcs/rudder-pos-rad
194    </COMPONENT>
195    <COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
196      INPUT   fcs/flap-cmd-norm
197      DETENTS 5
198              0   0
199              8   3
200              15  3
201              25  4
202              42  4
203      OUTPUT  fcs/flap-pos-deg
204    </COMPONENT>
205    <COMPONENT NAME="Gear Control" TYPE="KINEMAT">
206      INPUT   gear/gear-cmd-norm
207      DETENTS 2
208              0   0
209              1   5
210      OUTPUT  gear/gear-pos-norm
211    </COMPONENT>
212    <COMPONENT NAME="Speedbrake Control" TYPE="KINEMAT">
213      INPUT   fcs/speedbrake-cmd-norm
214      DETENTS 2
215              0   0
216              1   1
217      OUTPUT  fcs/speedbrake-pos-norm
218    </COMPONENT>
219    <COMPONENT NAME="Spoiler Control" TYPE="KINEMAT">
220      INPUT   fcs/spoiler-cmd-norm
221      DETENTS 2
222              0   0
223              1   1
224      OUTPUT  fcs/spoiler-pos-norm
225    </COMPONENT>
226    <COMPONENT NAME="Spoiler Control" TYPE="KINEMAT">
227      INPUT   fcs/spoiler-cmd-norm
228      DETENTS 2
229              0   0
230              1   1
231      OUTPUT  fcs/reverser-pos-norm
232    </COMPONENT>
233  </FLIGHT_CONTROL>
234  <AERODYNAMICS>
235   <AXIS NAME="LIFT">
236     <!-- aeromatic, Linssys, AD -->
237     <COEFFICIENT NAME="CLalpha" TYPE="VECTOR">
238       Lift_due_to_alpha
239       4
240       aero/alpha-rad
241       aero/qbar-psf|metrics/Sw-sqft
242       -0.20   -0.680
243        0.00    0.200
244        0.23    1.200
245        0.60    0.600
246     </COEFFICIENT>
247     <!-- AD, BH -->
248     <COEFFICIENT NAME="dCLflap" TYPE="VECTOR">
249        Delta_Lift_due_to_flaps
250        5
251        fcs/components/flaps-control/output-norm
252        aero/qbar-psf|metrics/Sw-sqft
253        0.000   0.000
254        0.190   0.598
255        0.357   0.960
256        0.595   1.390
257        1.000   2.250
258     </COEFFICIENT>
259     <!-- wild guess -->
260     <COEFFICIENT NAME="dCLsp" TYPE="VALUE">
261        Delta_Lift_due_to_spoiler
262        aero/qbar-psf|metrics/Sw-sqft|fcs/spoiler-pos-norm
263        -0.1
264     </COEFFICIENT>
265     <COEFFICIENT NAME="CLde" TYPE="VALUE">
266        Lift_due_to_Elevator_Deflection
267        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-rad
268        0.2
269     </COEFFICIENT>
270   </AXIS>
271   <!-- aeromatic, Linssys -->
272   <AXIS NAME="DRAG">
273     <COEFFICIENT NAME="CD0" TYPE="VECTOR">
274        Drag_at_zero_lift
275        5
276        aero/alpha-rad
277        aero/qbar-psf|metrics/Sw-sqft
278        -1.57       1.500
279        -0.26       0.040
280         0.00       0.01922
281         0.26       0.040
282         1.57       1.500
283     </COEFFICIENT>
284     <!-- Linssys -->
285     <COEFFICIENT NAME="CDi" TYPE="VALUE">
286        Induced_drag
287        aero/qbar-psf|metrics/Sw-sqft|aero/cl-squared-norm
288        0.04478
289     </COEFFICIENT>
290     <!-- Linssys -->
291     <COEFFICIENT NAME="CDcomp" TYPE="VALUE">
292        Drag_due_to_compressibility
293        aero/qbar-psf|metrics/Sw-sqft
294        0.00115
295     </COEFFICIENT>
296     <COEFFICIENT NAME="CDmach" TYPE="VECTOR">
297        Drag_due_to_mach
298        4
299        velocities/mach-norm
300        aero/qbar-psf|metrics/Sw-sqft
301        0.0       0.000
302        0.79      0.000
303        1.1       0.023
304        1.8       0.015
305     </COEFFICIENT>
306     <COEFFICIENT NAME="CDflap" TYPE="VALUE">
307        Drag_due_to_flaps
308        aero/qbar-psf|metrics/Sw-sqft|fcs/components/flaps-control/output-norm
309        0.083
310     </COEFFICIENT>
311     <COEFFICIENT NAME="CDgear" TYPE="VALUE">
312        Drag_due_to_gear
313        aero/qbar-psf|metrics/Sw-sqft|gear/gear-pos-norm
314        0.015
315     </COEFFICIENT>
316     <COEFFICIENT NAME="CDsb" TYPE="VALUE">
317        Drag_due_to_speedbrakes
318        aero/qbar-psf|metrics/Sw-sqft|fcs/speedbrake-pos-norm
319        0.08
320     </COEFFICIENT>
321     <!-- wild guess -->
322     <COEFFICIENT NAME="CDsp" TYPE="VALUE">
323        Drag_due_to_spoilers
324        aero/qbar-psf|metrics/Sw-sqft|fcs/spoiler-pos-norm
325        0.028
326     </COEFFICIENT>
327     <COEFFICIENT NAME="CDbeta" TYPE="VECTOR">
328        Drag_due_to_sideslip
329        5
330        aero/beta-rad
331        aero/qbar-psf|metrics/Sw-sqft
332        -1.57       1.230
333        -0.26       0.050
334         0.00       0.00
335         0.26       0.050
336         1.57       1.230
337     </COEFFICIENT>
338     <COEFFICIENT NAME="CDde" TYPE="VALUE">
339        Drag_due_to_Elevator_Deflection
340        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-norm
341        0.059
342     </COEFFICIENT>
343   </AXIS>
344   <AXIS NAME="SIDE">
345     <COEFFICIENT NAME="CYb" TYPE="VALUE">
346        Side_force_due_to_beta
347        aero/qbar-psf|metrics/Sw-sqft|aero/beta-rad
348        -1
349     </COEFFICIENT>
350   </AXIS>
351   <AXIS NAME="ROLL">
352     <COEFFICIENT NAME="Clb" TYPE="VALUE">
353        Roll_moment_due_to_beta
354        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
355        -0.1
356     </COEFFICIENT>
357     <COEFFICIENT NAME="Clp" TYPE="VALUE">
358        Roll_moment_due_to_roll_rate
359        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/p-aero-rad_sec
360        -0.4
361     </COEFFICIENT>
362     <COEFFICIENT NAME="Clr" TYPE="VALUE">
363        Roll_moment_due_to_yaw_rate
364        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
365        0.15
366     </COEFFICIENT>
367     <COEFFICIENT NAME="Clda" TYPE="VECTOR">
368        Roll_moment_due_to_aileron
369        2
370        velocities/mach-norm
371        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
372        0.0       0.1
373        2.0       0.033
374     </COEFFICIENT>
375     <COEFFICIENT NAME="Cldr" TYPE="VALUE">
376        Roll_moment_due_to_rudder
377        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
378        0.01
379     </COEFFICIENT>
380   </AXIS>
381   <AXIS NAME="PITCH">
382     <COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
383        Pitch_moment_due_to_alpha
384        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/alpha-rad
385        -0.6
386     </COEFFICIENT>
387     <COEFFICIENT NAME="Cmde" TYPE="VECTOR">
388        Pitch_moment_due_to_elevator
389        2
390        velocities/mach-norm
391        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|fcs/elevator-pos-rad
392        0.0       -1.2
393        2.0       -0.300
394     </COEFFICIENT>
395     <COEFFICIENT NAME="Cmq" TYPE="VALUE">
396        Pitch_moment_due_to_pitch_rate
397        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|velocities/q-aero-rad_sec
398        -17
399     </COEFFICIENT>
400     <COEFFICIENT NAME="Cmadot" TYPE="VALUE">
401        Pitch_moment_due_to_alpha_rate
402        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|aero/alphadot-rad_sec
403        -6
404     </COEFFICIENT>
405   </AXIS>
406   <AXIS NAME="YAW">
407     <COEFFICIENT NAME="Cnb" TYPE="VALUE">
408        Yaw_moment_due_to_beta
409        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
410        0.12
411     </COEFFICIENT>
412     <COEFFICIENT NAME="Cnr" TYPE="VALUE">
413        Yaw_moment_due_to_yaw_rate
414        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
415        -0.15
416     </COEFFICIENT>
417     <COEFFICIENT NAME="Cndr" TYPE="VALUE">
418        Yaw_moment_due_to_rudder
419        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
420        -0.1
421     </COEFFICIENT>
422     <COEFFICIENT NAME="Cnda" TYPE="VALUE">
423        Adverse_yaw
424        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
425        0
426     </COEFFICIENT>
427   </AXIS>
428  </AERODYNAMICS>
429 </FDM_CONFIG>
430