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Updated all JSBSim aircraft config files to new file format

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This commit is contained in:
tony 2002-09-24 12:56:05 +00:00
parent 37fb178385
commit d50ac80260
1 changed files with 64 additions and 72 deletions
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136
Aircraft/c172p/c172p.xml
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@ -1,4 +1,4 @@
<FDM_CONFIG NAME="c172" VERSION="1.58">
<FDM_CONFIG NAME="c172p" VERSION="1.60">
<!--
File: c172p.xml (originally c172.xml)
@ -116,7 +116,7 @@
FEED 1
</AC_ENGINE>
<AC_THRUSTER FILE="prop_generic2f">
<AC_THRUSTER FILE="prop_75in2f">
XLOC -37.7
YLOC 0.0
ZLOC 26.6
@ -149,65 +149,57 @@
<FLIGHT_CONTROL NAME="c172">
<COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
ID 0
INPUT FG_ELEVATOR_CMD
INPUT FG_PITCH_TRIM_CMD
INPUT fcs/elevator-cmd-norm
INPUT fcs/pitch-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
ID 1
INPUT 0
INPUT fcs/pitch-trim-sum
MIN -28
MAX 23
OUTPUT FG_ELEVATOR_POS
OUTPUT fcs/elevator-pos-rad
GAIN 0.01745
</COMPONENT>
<COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
ID 2
INPUT FG_AILERON_CMD
INPUT FG_ROLL_TRIM_CMD
INPUT fcs/aileron-cmd-norm
INPUT fcs/roll-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
ID 3
INPUT 2
INPUT fcs/roll-trim-sum
MIN -20
MAX 15
GAIN 0.01745
OUTPUT FG_LEFT_AILERON_POS
OUTPUT fcs/left-aileron-pos-rad
</COMPONENT>
<COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
ID 4
INPUT 2
INPUT fcs/roll-trim-sum
MIN -20
MAX 15
INVERT
GAIN 0.01745
OUTPUT FG_RIGHT_AILERON_POS
OUTPUT fcs/right-aileron-pos-rad
</COMPONENT>
<COMPONENT NAME="Yaw Trim Sum" TYPE="SUMMER">
ID 5
INPUT FG_RUDDER_CMD
INPUT FG_YAW_TRIM_CMD
INPUT fcs/rudder-cmd-norm
INPUT fcs/yaw-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
ID 6
INPUT 5
INPUT fcs/yaw-trim-sum
MIN -16
MAX 16
GAIN 0.01745
OUTPUT FG_RUDDER_POS
OUTPUT fcs/rudder-pos-rad
</COMPONENT>
<COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
ID 7
INPUT FG_FLAPS_CMD
INPUT fcs/flap-cmd-norm
DETENTS 4
0 0
10 2
20 1
30 1
OUTPUT FG_FLAPS_POS
OUTPUT fcs/flap-pos-deg
</COMPONENT>
</FLIGHT_CONTROL>
@ -222,8 +214,8 @@
<FACTOR NAME="kCLge" TYPE="VECTOR">
Change_in_lift_due_to_ground_effect
13
FG_HOVERB
FG_NONE
aero/h_b-mac-ft
none
0.0 1.203
0.1 1.127
0.15 1.090
@ -242,9 +234,9 @@
Lift_due_to_alpha
17
2
FG_ALPHA
FG_HYSTPARM
FG_QBAR|FG_WINGAREA
aero/alpha-rad
aero/stall-hyst-norm
aero/qbar-psf | metrics/Sw-sqft
0 1
-0.09 -0.22 -0.22
0 0.25 0.25
@ -267,8 +259,8 @@
<COEFFICIENT NAME="CLDf" TYPE="VECTOR">
Delta_lift_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
fcs/flap-pos-deg
aero/qbar-psf | metrics/Sw-sqft
0 0
10 0.20
20 0.30
@ -277,24 +269,24 @@
</GROUP>
<COEFFICIENT NAME="CLDe" TYPE="VALUE">
Lift_due_to_Elevator_Deflection
FG_QBAR|FG_WINGAREA|FG_ELEVATOR_POS
aero/qbar-psf | metrics/Sw-sqft | fcs/elevator-pos-rad
0.347
</COEFFICIENT>
<COEFFICIENT NAME="CLadot" TYPE="VALUE">
Lift_due_to_alpha_rate
FG_QBAR|FG_WINGAREA|FG_ALPHADOT|FG_CI2VEL
aero/qbar-psf | metrics/Sw-sqft | aero/alphadot-rad_sec | aero/ci2vel
1.7
</COEFFICIENT>
<COEFFICIENT NAME="CLq" TYPE="VALUE">
Lift_due_to_pitch_rate
FG_QBAR|FG_WINGAREA|FG_AEROQ|FG_CI2VEL
aero/qbar-psf | metrics/Sw-sqft | velocities/q-aero-rad_sec | aero/ci2vel
3.9
</COEFFICIENT>
</AXIS>
<AXIS NAME="DRAG">
<COEFFICIENT NAME="CDo" TYPE="VALUE">
Drag_at_zero_lift
FG_QBAR|FG_WINGAREA
aero/qbar-psf | metrics/Sw-sqft
0.026
</COEFFICIENT>
<GROUP NAME="CDb">
@ -302,8 +294,8 @@
<FACTOR NAME="kCDge" TYPE="VECTOR">
Change_in_drag_due_to_ground_effect
13
FG_HOVERB
FG_NONE
aero/h_b-mac-ft
none
0.0 0.048
0.1 0.515
0.15 0.629
@ -321,8 +313,8 @@
<COEFFICIENT NAME="CDDf" TYPE="VECTOR">
Delta_drag_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
fcs/flap-pos-deg
aero/qbar-psf | metrics/Sw-sqft
0 0
10 0.007
20 0.012
@ -332,9 +324,9 @@
Drag_due_to_alpha
26
4
FG_ALPHA
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
aero/alpha-rad
fcs/flap-pos-deg
aero/qbar-psf | metrics/Sw-sqft
0 10 20 30
-0.0872664 0.00407143 3.8165e-05 0.000512444 0.00137231
-0.0698132 0.0013424 0.000440634 0.00248067 0.00412341
@ -366,12 +358,12 @@
</GROUP>
<COEFFICIENT NAME="CDDe" TYPE="VALUE">
Drag_due_to_Elevator_Deflection
FG_QBAR|FG_WINGAREA|FG_AELEVATOR_POS
aero/qbar-psf | metrics/Sw-sqft | fcs/mag-elevator-pos-rad
0.06
</COEFFICIENT>
<COEFFICIENT NAME="CDbeta" TYPE="VALUE">
Drag_due_to_sideslip
FG_QBAR|FG_WINGAREA|FG_ABETA
aero/qbar-psf | metrics/Sw-sqft | aero/mag-beta-rad
0.17
</COEFFICIENT>
@ -381,8 +373,8 @@
<COEFFICIENT NAME="CYb" TYPE="VECTOR">
Side_force_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA
aero/beta-rad
aero/qbar-psf | metrics/Sw-sqft
-0.349 0.108
0 0
0.349 -0.108
@ -390,23 +382,23 @@
<COEFFICIENT NAME="CYda" TYPE="VALUE">
Side_force_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_AILERON_POS
aero/qbar-psf | metrics/Sw-sqft | fcs/left-aileron-pos-rad
-0.05
</COEFFICIENT>
<COEFFICIENT NAME="CYdr" TYPE="VALUE">
Side_force_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_RUDDER_POS
aero/qbar-psf | metrics/Sw-sqft | fcs/rudder-pos-rad
0.098
</COEFFICIENT>
<COEFFICIENT NAME="CYp" TYPE="VALUE">
Side_force_due_to_roll_rate
FG_QBAR|FG_WINGAREA|FG_BI2VEL|FG_AEROP
aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/p-aero-rad_sec
-0.037
</COEFFICIENT>
<COEFFICIENT NAME="CYr" TYPE="VALUE">
Side_force_due_to_yaw_rate
FG_QBAR|FG_WINGAREA|FG_BI2VEL|FG_AEROR
aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/r-aero-rad_sec
0.21
</COEFFICIENT>
</AXIS>
@ -415,8 +407,8 @@
<COEFFICIENT NAME="Clb" TYPE="VECTOR">
Roll_moment_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN
aero/beta-rad
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft
-0.349 0.0311
0 0
0.349 -0.0311
@ -424,28 +416,28 @@
<COEFFICIENT NAME="Clp" TYPE="VALUE">
Roll_moment_due_to_roll_rate_(roll_damping)
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROP
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec
-0.47
</COEFFICIENT>
<COEFFICIENT NAME="Clr" TYPE="VECTOR">
Roll_moment_due_to_yaw_rate
2
FG_ALPHA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROR
aero/alpha-rad
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec
0.000 0.08
0.094 0.19
</COEFFICIENT>
<COEFFICIENT NAME="Clda" TYPE="VALUE">
Roll_moment_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_AILERON_POS
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad
0.23
</COEFFICIENT>
<COEFFICIENT NAME="Cldr" TYPE="VALUE">
Roll_moment_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_RUDDER_POS
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad
0.0147
</COEFFICIENT>
@ -455,14 +447,14 @@
<COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
Pitch_moment_due_to_alpha
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_ALPHA
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/alpha-rad
-1.8
</COEFFICIENT>
<COEFFICIENT NAME="CmDf" TYPE="VECTOR">
Delta_pitching_moment_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA|FG_CBAR
fcs/flap-pos-deg
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft
0 0
10 -0.0654
20 -0.0981
@ -470,23 +462,23 @@
</COEFFICIENT>
<COEFFICIENT NAME="Cmq" TYPE="VALUE">
Pitch_moment_due_to_pitch_rate
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_CI2VEL|FG_AEROQ
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | velocities/q-aero-rad_sec
-12.4
</COEFFICIENT>
<COEFFICIENT NAME="Cmadot" TYPE="VALUE">
Pitch_moment_due_to_alpha_rate
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_CI2VEL|FG_ALPHADOT
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | aero/alphadot-rad_sec
-5.2
</COEFFICIENT>
<COEFFICIENT NAME="Cmo" TYPE="VALUE">
Pitching_moment_at_zero_alpha
FG_QBAR|FG_WINGAREA|FG_CBAR
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft
0.1
</COEFFICIENT>
<COEFFICIENT NAME="Cmde" TYPE="VALUE">
Pitch_moment_due_to_elevator_deflection
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_ELEVATOR_POS
aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | fcs/elevator-pos-rad
-1.28
</COEFFICIENT>
@ -497,33 +489,33 @@
<COEFFICIENT NAME="Cnb" TYPE="VECTOR">
Yaw_moment_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN
aero/beta-rad
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft
-0.349 -0.0227
0 0
0.349 0.0227
</COEFFICIENT>
<COEFFICIENT NAME="Cnp" TYPE="VALUE">
Yaw_moment_due_to_roll_rate
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROP
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec
-0.03
</COEFFICIENT>
<COEFFICIENT NAME="Cnr" TYPE="VALUE">
Yaw_moment_due_to_yaw_rate
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROR
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec
-0.099
</COEFFICIENT>
<COEFFICIENT NAME="Cnda" TYPE="VALUE">
Yaw_moment_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_AILERON_POS
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad
0.0053
</COEFFICIENT>
<COEFFICIENT NAME="Cndr" TYPE="VALUE">
Yaw_moment_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_RUDDER_POS
aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad
-0.043
</COEFFICIENT>