David Culp:
[fg:fgdata.git] / Aircraft / sgs233 / sgs233.xml
1 <FDM_CONFIG NAME="sgs233" VERSION="1.65" RELEASE="BETA">
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 -25.8 700 140 0.5 0.8 0.5 FIXED NONE 0 RETRACT
49   AC_GEAR RIGHT_MLG  108.36 2.4 -25.8 700 140 0.5 0.8 0.5 FIXED NONE 0 RETRACT
50   AC_GEAR NOSE_LG   33.54 0 -15.48 210 70 0.5 0.8 0.5 STEERABLE NONE 5 RETRACT
51   AC_GEAR LEFT_WING 103.2 -20 -6.45 210 70 0.5 0.8 0.5 FIXED NONE 0 RETRACT
52   AC_GEAR RIGHT_WING 103.2 -20 -6.45 210 70 0.5 0.8 0.5 FIXED NONE 0 RETRACT
53  </UNDERCARRIAGE>
54  <PROPULSION>
55  </PROPULSION>
56  <FLIGHT_CONTROL NAME="sgs233">
57    <COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
58       INPUT   fcs/elevator-cmd-norm
59       INPUT   fcs/pitch-trim-cmd-norm
60       CLIPTO  -1 1
61    </COMPONENT>
62    <COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
63       INPUT   fcs/pitch-trim-sum
64       MIN     -0.350
65       MAX      0.300
66       OUTPUT  fcs/elevator-pos-rad
67    </COMPONENT>
68    <COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
69       INPUT   fcs/aileron-cmd-norm
70       INPUT   fcs/roll-trim-cmd-norm
71       CLIPTO  -1 1
72    </COMPONENT>
73    <COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
74       INPUT   fcs/roll-trim-sum
75       MIN    -0.35
76       MAX     0.35
77       OUTPUT  fcs/left-aileron-pos-rad
78    </COMPONENT>
79    <COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
80       INPUT  -fcs/roll-trim-sum
81       MIN    -0.35
82       MAX     0.35
83       OUTPUT  fcs/right-aileron-pos-rad
84    </COMPONENT>
85    <COMPONENT NAME="Rudder Command Sum" TYPE="SUMMER">
86       INPUT   fcs/rudder-cmd-norm
87       INPUT   fcs/yaw-trim-cmd-norm
88       CLIPTO  -1 1
89    </COMPONENT>
90    <COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
91       INPUT   fcs/rudder-command-sum
92       MIN     -0.35
93       MAX      0.35
94       OUTPUT  fcs/rudder-pos-rad
95    </COMPONENT>
96    <COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
97      INPUT   fcs/flap-cmd-norm
98      DETENTS 3
99              0   0
100              15  4
101              30  3
102      OUTPUT  fcs/flap-pos-deg
103    </COMPONENT>
104    <COMPONENT NAME="Gear Control" TYPE="KINEMAT">
105      INPUT   gear/gear-cmd-norm
106      DETENTS 2
107              0   0
108              1   5
109      OUTPUT  gear/gear-pos-norm
110    </COMPONENT>
111    <COMPONENT NAME="Speedbrake Control" TYPE="KINEMAT">
112      INPUT   fcs/speedbrake-cmd-norm
113      DETENTS 2
114              0   0
115              1   1
116      OUTPUT  fcs/speedbrake-pos-norm
117    </COMPONENT>
118  </FLIGHT_CONTROL>
119  <AERODYNAMICS>
120   <AXIS NAME="LIFT">
121     <COEFFICIENT NAME="CLalpha" TYPE="VECTOR">
122       Lift_due_to_alpha
123       4
124       aero/alpha-rad
125       aero/qbar-psf|metrics/Sw-sqft
126       -0.20   -0.850
127        0.00    0.250
128        0.21    1.400
129        0.60    0.710
130     </COEFFICIENT>
131     <COEFFICIENT NAME="dCLsb" TYPE="VALUE">
132        Delta_Lift_due_to_speedbrake
133        aero/qbar-psf|metrics/Sw-sqft|fcs/speedbrake-pos-norm
134        -0.05
135     </COEFFICIENT>
136     <COEFFICIENT NAME="CLde" TYPE="VALUE">
137        Lift_due_to_Elevator_Deflection
138        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-rad
139        0.2
140     </COEFFICIENT>
141   </AXIS>
142   <AXIS NAME="DRAG">
143     <COEFFICIENT NAME="CD0" TYPE="VECTOR">
144        Drag_at_zero_lift
145        5
146        aero/alpha-rad
147        aero/qbar-psf|metrics/Sw-sqft
148        -1.57       1.500
149        -0.26       0.020
150         0.00       0.010
151         0.26       0.020
152         1.57       1.500
153     </COEFFICIENT>
154     <COEFFICIENT NAME="CDi" TYPE="VALUE">
155        Induced_drag
156        aero/qbar-psf|metrics/Sw-sqft|aero/cl-squared-norm
157        0.023
158     </COEFFICIENT>
159     <COEFFICIENT NAME="CDmach" TYPE="VECTOR">
160        Drag_due_to_mach
161        4
162        velocities/mach-norm
163        aero/qbar-psf|metrics/Sw-sqft
164        0.0       0.000
165        0.7       0.000
166        1.1       0.023
167        1.8       0.015
168     </COEFFICIENT>
169     <COEFFICIENT NAME="CDflap" TYPE="VALUE">
170        Drag_due_to_flaps
171        aero/qbar-psf|metrics/Sw-sqft|fcs/components/flaps-control/output-norm
172        0.024
173     </COEFFICIENT>
174     <COEFFICIENT NAME="CDgear" TYPE="VALUE">
175        Drag_due_to_gear
176        aero/qbar-psf|metrics/Sw-sqft|gear/gear-pos-norm
177        0.001
178     </COEFFICIENT>
179     <COEFFICIENT NAME="CDsb" TYPE="VALUE">
180        Drag_due_to_speedbrakes
181        aero/qbar-psf|metrics/Sw-sqft|fcs/speedbrake-pos-norm
182        0.01
183     </COEFFICIENT>
184     <COEFFICIENT NAME="CDbeta" TYPE="VECTOR">
185        Drag_due_to_sideslip
186        5
187        aero/beta-rad
188        aero/qbar-psf|metrics/Sw-sqft
189        -1.57       1.230
190        -0.26       0.050
191         0.00       0.00
192         0.26       0.050
193         1.57       1.230
194     </COEFFICIENT>
195     <COEFFICIENT NAME="CDde" TYPE="VALUE">
196        Drag_due_to_Elevator_Deflection
197        aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-norm
198        0.024
199     </COEFFICIENT>
200   </AXIS>
201   <AXIS NAME="SIDE">
202     <COEFFICIENT NAME="CYb" TYPE="VALUE">
203        Side_force_due_to_beta
204        aero/qbar-psf|metrics/Sw-sqft|aero/beta-rad
205        -1
206     </COEFFICIENT>
207   </AXIS>
208   <AXIS NAME="ROLL">
209     <COEFFICIENT NAME="Clb" TYPE="VALUE">
210        Roll_moment_due_to_beta
211        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
212        -0.1
213     </COEFFICIENT>
214     <COEFFICIENT NAME="Clp" TYPE="VALUE">
215        Roll_moment_due_to_roll_rate
216        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/p-aero-rad_sec
217        -0.4
218     </COEFFICIENT>
219     <COEFFICIENT NAME="Clr" TYPE="VALUE">
220        Roll_moment_due_to_yaw_rate
221        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
222        0.15
223     </COEFFICIENT>
224     <COEFFICIENT NAME="Clda" TYPE="VECTOR">
225        Roll_moment_due_to_aileron
226        2
227        velocities/mach-norm
228        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
229        0.0       0.06
230        2.0       0.020
231     </COEFFICIENT>
232     <COEFFICIENT NAME="Cldr" TYPE="VALUE">
233        Roll_moment_due_to_rudder
234        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
235        0.01
236     </COEFFICIENT>
237   </AXIS>
238   <AXIS NAME="PITCH">
239     <COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
240        Pitch_moment_due_to_alpha
241        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/alpha-rad
242        -0.5
243     </COEFFICIENT>
244     <COEFFICIENT NAME="Cmde" TYPE="VECTOR">
245        Pitch_moment_due_to_elevator
246        2
247        velocities/mach-norm
248        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|fcs/elevator-pos-rad
249        0.0       -0.8
250        2.0       -0.200
251     </COEFFICIENT>
252     <COEFFICIENT NAME="Cmq" TYPE="VALUE">
253        Pitch_moment_due_to_pitch_rate
254        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|velocities/q-aero-rad_sec
255        -9
256     </COEFFICIENT>
257     <COEFFICIENT NAME="Cmadot" TYPE="VALUE">
258        Pitch_moment_due_to_alpha_rate
259        aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|aero/alphadot-rad_sec
260        -12
261     </COEFFICIENT>
262   </AXIS>
263   <AXIS NAME="YAW">
264     <COEFFICIENT NAME="Cnb" TYPE="VALUE">
265        Yaw_moment_due_to_beta
266        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
267        0.12
268     </COEFFICIENT>
269     <COEFFICIENT NAME="Cnr" TYPE="VALUE">
270        Yaw_moment_due_to_yaw_rate
271        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
272        -0.15
273     </COEFFICIENT>
274     <COEFFICIENT NAME="Cndr" TYPE="VALUE">
275        Yaw_moment_due_to_rudder
276        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
277        -0.03
278     </COEFFICIENT>
279     <COEFFICIENT NAME="Cnda" TYPE="VALUE">
280        Adverse_yaw
281        aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
282        -0.02
283     </COEFFICIENT>
284   </AXIS>
285  </AERODYNAMICS>
286 </FDM_CONFIG>