David Culp:
[fg:fgdata.git] / Aircraft / sgs233 / sgs233.xml
1 <FDM_CONFIG NAME="sgs233" VERSION="1.65" >
2 <!--
3   File:     sgs233.xml
4   Author:   Aero-Matic v 0.7
5
6   Inputs:
7     name:          sgs233
8     type:          glider
9     max weight:    1040.0 lb
10     wing span:     51.0 ft
11     length:        25.7 ft
12     wing area:     219.48 sq-ft
13     gear type:     tricycle
14     retractable?:  yes
15     # engines:     0
16     engine type:   piston
17     engine layout: forward fuselage
18     yaw damper?    no
19
20   Outputs:
21     wing loading:   4.73 lb/sq-ft
22     CL-alpha:      5.5 per radian
23     CL-0:          0.25
24     CL-max:        1.4
25     CD-0:          0.01
26     K:             0.023
27
28 -->
29
30  <METRICS>
31    AC_WINGAREA  219.48
32    AC_WINGSPAN  51.00
33    AC_CHORD      4.30
34    AC_HTAILAREA 24.00
35    AC_HTAILARM  14.00
36    AC_VTAILAREA 18.00
37    AC_LV        14.00
38    AC_IXX       1800
39    AC_IYY       700
40    AC_IZZ       1950
41    AC_IXZ       0
42    AC_EMPTYWT   610
43    AC_CGLOC     103.2  0.0 -6.4
44    AC_AERORP    103.2  0.0  0.0
45    AC_EYEPTLOC  49.0  0.0  9.0
46  </METRICS>
47  <UNDERCARRIAGE>
48   AC_GEAR LEFT_MLG   108.36  -2.4 -50.0 700 140 0.5 0.8 0.05 FIXED NONE 0 RETRACT
49   AC_GEAR RIGHT_MLG  108.36   2.4 -50.0 700 140 0.5 0.8 0.05 FIXED NONE 0 RETRACT
50   AC_GEAR NOSE_LG     33.54   0   -48.0 210  70 0.5 0.8 0.5  STEERABLE NONE 5 RETRACT
51   AC_GEAR LEFT_WING  103.2 -240     6.0 210  70 0.5 0.8 0.5  FIXED NONE 0 RETRACT
52   AC_GEAR RIGHT_WING 103.2  240     6.0 210  70 0.5 0.8 0.5  FIXED NONE 0 RETRACT
53   AC_GEAR TAIL       271.0    0   -20.0 210  70 0.5 0.8 0.5  FIXED NONE 0 RETRACT
54  </UNDERCARRIAGE>
55  <PROPULSION>
56  </PROPULSION>
57  <FLIGHT_CONTROL NAME="sgs233">
58    <COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
59       INPUT   fcs/elevator-cmd-norm
60       INPUT   fcs/pitch-trim-cmd-norm
61       CLIPTO  -1 1
62    </COMPONENT>
63    <COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
64       INPUT   fcs/pitch-trim-sum
65       MIN     -0.350
66       MAX      0.300
67       OUTPUT  fcs/elevator-pos-rad
68    </COMPONENT>
69    <COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
70       INPUT   fcs/aileron-cmd-norm
71       INPUT   fcs/roll-trim-cmd-norm
72       CLIPTO  -1 1
73    </COMPONENT>
74    <COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
75       INPUT   fcs/roll-trim-sum
76       MIN    -0.35
77       MAX     0.35
78       OUTPUT  fcs/left-aileron-pos-rad
79    </COMPONENT>
80    <COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
81       INPUT  -fcs/roll-trim-sum
82       MIN    -0.35
83       MAX     0.35
84       OUTPUT  fcs/right-aileron-pos-rad
85    </COMPONENT>
86    <COMPONENT NAME="Rudder Command Sum" TYPE="SUMMER">
87       INPUT   fcs/rudder-cmd-norm
88       INPUT   fcs/yaw-trim-cmd-norm
89       CLIPTO  -1 1
90    </COMPONENT>
91    <COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
92       INPUT   fcs/rudder-command-sum
93       MIN     -0.35
94       MAX      0.35
95       OUTPUT  fcs/rudder-pos-rad
96    </COMPONENT>
97    <COMPONENT NAME="Spoiler Control" TYPE="AEROSURFACE_SCALE">
98       INPUT   fcs/spoiler-cmd-norm
99       MIN     0
100       MAX     1.04895 
101       OUTPUT  fcs/spoiler-pos-rad
102    </COMPONENT>
103    <COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
104      INPUT   fcs/flap-cmd-norm
105      DETENTS 3
106              0   0
107              15  4
108              30  3
109      OUTPUT  fcs/flap-pos-deg
110    </COMPONENT>
111    <COMPONENT NAME="Gear Control" TYPE="KINEMAT">
112      INPUT   gear/gear-cmd-norm
113      DETENTS 2
114              0   0
115              1   5
116      OUTPUT  gear/gear-pos-norm
117    </COMPONENT>
118    <COMPONENT NAME="Speedbrake Control" TYPE="KINEMAT">
119      INPUT   fcs/speedbrake-cmd-norm
120      DETENTS 2
121              0   0
122              1   1
123      OUTPUT  fcs/speedbrake-pos-norm
124    </COMPONENT>
125  </FLIGHT_CONTROL>
126  <AERODYNAMICS>
127   <AXIS NAME="LIFT">
128     <COEFFICIENT NAME="CLalpha" TYPE="VECTOR">
129       Lift_due_to_alpha
130       4
131       aero/alpha-rad
132       aero/qbar-psf|metrics/Sw-sqft
133       -0.20   -0.850
134        0.00    0.250
135        0.21    1.400
136        0.60    0.710
137     </COEFFICIENT>
138     <COEFFICIENT NAME="dCLsp" TYPE="VALUE">
139        Delta_Lift_due_to_spoilers
140        aero/qbar-psf|metrics/Sw-sqft|fcs/spoiler-pos-rad
141        -0.08
142     </COEFFICIENT>
143     <COEFFICIENT NAME="CLde" TYPE="VALUE">
144        Lift_due_to_Elevator_Deflection
145        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-rad
146        0.2
147     </COEFFICIENT>
148   </AXIS>
149   <AXIS NAME="DRAG">
150     <COEFFICIENT NAME="CD0" TYPE="VECTOR">
151        Drag_at_zero_lift
152        5
153        aero/alpha-rad
154        aero/qbar-psf|metrics/Sw-sqft
155        -1.57       1.500
156        -0.26       0.020
157         0.00       0.010
158         0.26       0.020
159         1.57       1.500
160     </COEFFICIENT>
161     <COEFFICIENT NAME="CDi" TYPE="VALUE">
162        Induced_drag
163        aero/qbar-psf|metrics/Sw-sqft|aero/cl-squared-norm
164        0.023
165     </COEFFICIENT>
166     <COEFFICIENT NAME="CDmach" TYPE="VECTOR">
167        Drag_due_to_mach
168        4
169        velocities/mach-norm
170        aero/qbar-psf|metrics/Sw-sqft
171        0.0       0.000
172        0.7       0.000
173        1.1       0.023
174        1.8       0.015
175     </COEFFICIENT>
176     <COEFFICIENT NAME="CDflap" TYPE="VALUE">
177        Drag_due_to_flaps
178        aero/qbar-psf|metrics/Sw-sqft|fcs/components/flaps-control/output-norm
179        0.024
180     </COEFFICIENT>
181     <COEFFICIENT NAME="CDgear" TYPE="VALUE">
182        Drag_due_to_gear
183        aero/qbar-psf|metrics/Sw-sqft|gear/gear-pos-norm
184        0.001
185     </COEFFICIENT>
186     <COEFFICIENT NAME="CDsp" TYPE="VALUE">
187        Drag_due_to_spoilers
188        aero/qbar-psf|metrics/Sw-sqft|fcs/spoiler-pos-rad
189        0.02
190     </COEFFICIENT>
191     <COEFFICIENT NAME="CDbeta" TYPE="VECTOR">
192        Drag_due_to_sideslip
193        5
194        aero/beta-rad
195        aero/qbar-psf|metrics/Sw-sqft
196        -1.57       1.230
197        -0.26       0.050
198         0.00       0.00
199         0.26       0.050
200         1.57       1.230
201     </COEFFICIENT>
202     <COEFFICIENT NAME="CDde" TYPE="VALUE">
203        Drag_due_to_Elevator_Deflection
204        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-norm
205        0.024
206     </COEFFICIENT>
207   </AXIS>
208   <AXIS NAME="SIDE">
209     <COEFFICIENT NAME="CYb" TYPE="VALUE">
210        Side_force_due_to_beta
211        aero/qbar-psf|metrics/Sw-sqft|aero/beta-rad
212        -1
213     </COEFFICIENT>
214   </AXIS>
215   <AXIS NAME="ROLL">
216     <COEFFICIENT NAME="Clb" TYPE="VALUE">
217        Roll_moment_due_to_beta
218        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
219        -0.1
220     </COEFFICIENT>
221     <COEFFICIENT NAME="Clp" TYPE="VALUE">
222        Roll_moment_due_to_roll_rate
223        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/p-aero-rad_sec
224        -0.4
225     </COEFFICIENT>
226     <COEFFICIENT NAME="Clr" TYPE="VALUE">
227        Roll_moment_due_to_yaw_rate
228        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
229        0.15
230     </COEFFICIENT>
231     <COEFFICIENT NAME="Clda" TYPE="VECTOR">
232        Roll_moment_due_to_aileron
233        2
234        velocities/mach-norm
235        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
236        0.0       0.06
237        2.0       0.020
238     </COEFFICIENT>
239     <COEFFICIENT NAME="Cldr" TYPE="VALUE">
240        Roll_moment_due_to_rudder
241        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
242        0.01
243     </COEFFICIENT>
244   </AXIS>
245   <AXIS NAME="PITCH">
246     <COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
247        Pitch_moment_due_to_alpha
248        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/alpha-rad
249        -0.5
250     </COEFFICIENT>
251     <COEFFICIENT NAME="Cmde" TYPE="VECTOR">
252        Pitch_moment_due_to_elevator
253        2
254        velocities/mach-norm
255        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|fcs/elevator-pos-rad
256        0.0       -0.8
257        2.0       -0.200
258     </COEFFICIENT>
259     <COEFFICIENT NAME="Cmq" TYPE="VALUE">
260        Pitch_moment_due_to_pitch_rate
261        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|velocities/q-aero-rad_sec
262        -9
263     </COEFFICIENT>
264     <COEFFICIENT NAME="Cmadot" TYPE="VALUE">
265        Pitch_moment_due_to_alpha_rate
266        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|aero/alphadot-rad_sec
267        -12
268     </COEFFICIENT>
269   </AXIS>
270   <AXIS NAME="YAW">
271     <COEFFICIENT NAME="Cnb" TYPE="VALUE">
272        Yaw_moment_due_to_beta
273        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
274        0.12
275     </COEFFICIENT>
276     <COEFFICIENT NAME="Cnr" TYPE="VALUE">
277        Yaw_moment_due_to_yaw_rate
278        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
279        -0.15
280     </COEFFICIENT>
281     <COEFFICIENT NAME="Cndr" TYPE="VALUE">
282        Yaw_moment_due_to_rudder
283        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
284        -0.03
285     </COEFFICIENT>
286     <COEFFICIENT NAME="Cnda" TYPE="VALUE">
287        Adverse_yaw
288        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
289        -0.02
290     </COEFFICIENT>
291   </AXIS>
292  </AERODYNAMICS>
293 </FDM_CONFIG>