diff --git a/MQ-9-JSBSim2.xml b/MQ-9-JSBSim2.xml
index 0dc1a7c..f51c2e0 100644
--- a/MQ-9-JSBSim2.xml
+++ b/MQ-9-JSBSim2.xml
@@ -15,150 +15,86 @@
File: MQ-9 Reaper.xml
Inputs:
name: MQ-9 Reaper
- type: WWII fighter, subsonic sport, aerobatic
- max weight: 10495.8 lb
- wing span: 65.62 ft
- length: 36.091 ft
- wing area: 257.2825679 sq-ft
+ type: light commuter with 1 engines
+ stall speed: 80.00kts
+ max weight: 10494.00 lb
+ length: 36.08 ft
+ wing:
+ span: 65.58 ft
+ area: 257.28 sq-ft
+ mean chord: 3.92 ft
+ aspect ratio: 12.00:1
+ taper ratio: 1.00:1
+ incidence: 2.00 degrees
+ dihedral: 2.00 degrees
+ sweep: 5.00 degrees
+
+ no. engines: 1
+ engine type: Turboprop Engine
+ engine layout: aft fuselage
+
gear type: tricycle
+ steering type: steering
retractable?: yes
- # engines: 1
- engine type: turboprop
- engine layout: aft fuselage
- yaw damper? yes
+
Outputs:
wing loading: 40.79 lb/sq-ft
- payload: 4313.6 lbs
- CL-alpha: 4.5 per radian
- CL-0: 0.17
- CL-max: 1.2
+ payload: 4039.89 lbs
+ CL-alpha: 5.79 per radian
+ CL-0: 0.41
+ CL-max: 1.88
CD-0: 0.02
- K: 0.06
+ K: 0.04
+ Mcrit: 0.70
-->
- 257.28
- 65.62
- 2.00
- 3.92
- 32.29
- 21.65
- 10.76
- 21.65
+ 257.28
+ 65.58
+ 2.00
+ 3.92
+ 41.17
+ 18.76
+ 25.73
+ 18.04
- 173.24
- 0.00
- 0.00
+ 207.84
+ 0.00
+ 0.00
- 121.27
- 0.00
- 40.00
+ 56.29
+ -18.00
+ 45.00
- 0
- 0
- 0
+ 0.0
+ 0.0
+ 0.0
- 11946
- 6424
- 17362
- 4902
+ 11931.18
+ 6420.77
+ 17344.61
+ 4901.00
- 173.24
- 0.00
- -10.83
+ 207.84
+ 0.00
+ -10.82
- 4314 LBS + full (1280 LBS) fuel should bring model up to entered max weight
- 2156.8
+ 4039.89 LBS should bring model up to entered max weight
+ 2019.94
- 173.24
+ 207.84
0.00
- -10.83
+ -10.82
-
-
-
-
- 56.30
- 0.00
- -51.97
-
- 0.80
- 0.50
- 0.02
- 3148.74
- 5247.90
- 5.00
- NONE
- 1
-
-
-
-
- 180.17
- -118.12
- -51.97
-
- 0.80
- 0.50
- 0.02
- 10495.80
- 5247.90
- 0
- LEFT
- 1
-
-
-
-
- 180.17
- 118.12
- -51.97
-
- 0.80
- 0.50
- 0.02
- 10495.80
- 5247.90
- 0
- RIGHT
- 1
-
-
-
-
- 173.24
- -32.81
- -10.83
-
- 1.00
- 1.00
- 10495.80
- 10495.80
-
-
-
-
- 173.24
- 32.81
- -10.83
-
- 1.00
- 1.00
- 10495.80
- 10495.80
-
-
-
-
@@ -189,255 +125,106 @@
- 173.24
+ 207.84
0.00
-10.83
- 2000.00
- 1000.00
+ 776.56
+ 388.28
- 173.24
+ 207.84
0.00
-10.83
- 2000.00
- 1000.00
+ 776.56
+ 388.28
+
+
+
+
+
+ 56.29
+ 0.00
+ -51.96
+
+ 0.80
+ 0.50
+ 0.02
+ 3148.20
+ 1574.10
+ 5.00
+ NONE
+ 1
+
+
+
+
+ 216.15
+ -70.83
+ -51.96
+
+ 0.80
+ 0.50
+ 0.02
+ 10494.00
+ 5247.00
+ 0
+ LEFT
+ 1
+
+
+
+
+ 216.15
+ 70.83
+ -51.96
+
+ 0.80
+ 0.50
+ 0.02
+ 10494.00
+ 5247.00
+ 0
+ RIGHT
+ 1
+
+
+
+
+ 207.84
+ -393.50
+ -10.82
+
+ 1
+ 1
+ 10494.00
+ 10494.00
+
+
+
+
+ 207.84
+ 393.50
+ -10.82
+
+ 1
+ 1
+ 10494.00
+ 10494.00
+
+
+
+
-
-
-
-
-
- fcs/elevator-cmd-norm
- fcs/pitch-trim-cmd-norm
-
- -1
- 1
-
-
-
-
- fcs/pitch-trim-sum
-
- -0.35
- 0.35
-
- fcs/elevator-pos-rad
-
-
-
- fcs/elevator-pos-rad
-
- -0.35
- 0.35
-
-
- -1
- 1
-
- fcs/elevator-pos-norm
-
-
-
-
-
-
-
- fcs/aileron-cmd-norm
- fcs/roll-trim-cmd-norm
-
- -1
- 1
-
-
-
-
- fcs/roll-trim-sum
-
- -0.35
- 0.35
-
- fcs/left-aileron-pos-rad
-
-
-
- fcs/roll-trim-sum
-
- -0.35
- 0.35
-
- fcs/right-aileron-pos-rad
-
-
-
- fcs/left-aileron-pos-rad
-
- -0.35
- 0.35
-
-
- -1
- 1
-
- fcs/left-aileron-pos-norm
-
-
-
- fcs/right-aileron-pos-rad
-
- -0.35
- 0.35
-
-
- -1
- 1
-
- fcs/right-aileron-pos-norm
-
-
-
-
- fcs/yaw-damper-enable
-
-
-
- fcs/rudder-cmd-norm
- fcs/yaw-trim-cmd-norm
-
- -1
- 1
-
-
-
-
- velocities/r-aero-rad_sec
-
- velocities/ve-kts
-
- 30 0.00
- 60 2.00
-
-
- fcs/yaw-damper-enable
-
-
-
- fcs/rudder-command-sum
- fcs/yaw-damper-rate
-
- -1.1
- 1.1
-
-
-
-
- fcs/rudder-sum
-
- -1.1
- 1.1
-
-
- -0.35
- 0.35
-
- fcs/rudder-pos-rad
-
-
-
- fcs/rudder-pos-rad
-
- -0.35
- 0.35
-
-
- -1
- 1
-
- fcs/rudder-pos-norm
-
-
-
-
-
-
- fcs/flap-cmd-norm
-
-
- 0
- 0
-
-
- 15
- 4
-
-
- 30
- 3
-
-
- fcs/flap-pos-deg
-
-
-
- fcs/flap-pos-deg
-
- 0
- 30
-
-
- 0
- 1
-
- fcs/flap-pos-norm
-
-
-
-
-
-
- gear/gear-cmd-norm
-
-
- 0
- 0
-
-
- 1
- 5
-
-
- gear/gear-pos-norm
-
-
-
-
-
-
- fcs/speedbrake-cmd-norm
-
-
- 0
- 0
-
-
- 1
- 1
-
-
- fcs/speedbrake-pos-norm
-
-
-
-
-
+
@@ -451,34 +238,36 @@
aero/alpha-rad
- -0.20 -0.730
- 0.00 0.170
- 0.23 1.200
- 0.60 0.582
+ -0.20 -0.7494
+ 0.00 0.4077
+ 0.25 1.8824
+ 0.60 0.9976
-
- Delta Lift due to flaps
-
- aero/qbar-psf
- metrics/Sw-sqft
- fcs/flap-pos-deg
- 0.01000
-
-
+
+ Lift due to pitch rate
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ velocities/q-aero-rad_sec
+ aero/ci2vel
+ 6.4704
+
+
-
- Delta Lift due to speedbrake
-
+
+ Lift due to alpha rate
+
aero/qbar-psf
metrics/Sw-sqft
- fcs/speedbrake-pos-norm
- 0
-
-
+ aero/alphadot-rad_sec
+ aero/ci2vel
+ 1.8487
+
+
Lift due to Elevator Deflection
@@ -486,7 +275,7 @@
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
- 0.2
+ 0.2732
@@ -502,11 +291,11 @@
aero/alpha-rad
- -1.57 1.500
- -0.26 0.026
- 0.00 0.020
- 0.26 0.026
- 1.57 1.500
+ -1.57 1.4089
+ -0.25 0.0508
+ 0.00 0.0219
+ 0.25 0.0508
+ 1.57 1.4089
@@ -518,7 +307,7 @@
aero/qbar-psf
metrics/Sw-sqft
aero/cl-squared
- 0.06
+ 0.0240
@@ -530,45 +319,15 @@
velocities/mach
- 0.00 0.000
- 0.75 0.000
- 1.10 0.023
- 1.80 0.015
+ 0.00 0.0000
+ 0.70 0.0000
+ 1.10 0.0230
+ 1.80 0.0150
-
- Drag due to flaps
-
- aero/qbar-psf
- metrics/Sw-sqft
- fcs/flap-pos-deg
- 0.00133
-
-
-
-
- Drag due to gear
-
- aero/qbar-psf
- metrics/Sw-sqft
- gear/gear-pos-norm
- 0.03
-
-
-
-
- Drag due to speedbrakes
-
- aero/qbar-psf
- metrics/Sw-sqft
- fcs/speedbrake-pos-norm
- 0.02
-
-
-
Drag due to sideslip
@@ -577,11 +336,11 @@
aero/beta-rad
- -1.57 1.230
- -0.26 0.050
- 0.00 0.000
- 0.26 0.050
- 1.57 1.230
+ -1.57 1.2300
+ -0.26 0.0500
+ 0.00 0.0000
+ 0.26 0.0500
+ 1.57 1.2300
@@ -592,83 +351,71 @@
aero/qbar-psf
metrics/Sw-sqft
- fcs/elevator-pos-norm
- 0.04
+ fcs/elevator-pos-rad
+ 0.0400
-
-
-
-
-
- Side force due to beta
-
+
+ Drag due to gear
+
aero/qbar-psf
metrics/Sw-sqft
- aero/beta-rad
- -1
-
+ gear/gear-pos-norm
+ 0.0300
+
-
+
-
- Roll moment due to beta
+
+ Side force due to beta
aero/qbar-psf
metrics/Sw-sqft
- metrics/bw-ft
aero/beta-rad
- -0.1
+ -0.2310
-
-
- Roll moment due to roll rate
+
+ Side force due to roll rate
aero/qbar-psf
metrics/Sw-sqft
- metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
- -0.4
+
+ aero/Re
+
+ 3372885 1.3390
+ 3710173 0.1141
+ 5059327 0.0507
+ 6689612 0.0290
+
+
-
- Roll moment due to yaw rate
+
+ Side force due to yaw rate
aero/qbar-psf
metrics/Sw-sqft
- metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
- 0.15
+ 0.1271
-
- Roll moment due to aileron
-
- aero/qbar-psf
- metrics/Sw-sqft
- metrics/bw-ft
- fcs/left-aileron-pos-rad
- 0.18
-
-
-
-
- Roll moment due to rudder
+
+ Side force due to rudder
aero/qbar-psf
metrics/Sw-sqft
- metrics/bw-ft
fcs/rudder-pos-rad
- 0.01
+ 0.1407
@@ -683,7 +430,7 @@
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
- -0.5
+ -2.3270
@@ -697,8 +444,8 @@
velocities/mach
- 0.0 -1.000
- 2.0 -0.250
+ 0.0 -2.0259
+ 2.0 -0.5065
@@ -712,7 +459,7 @@
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
- -15
+ -30.9711
@@ -724,7 +471,90 @@
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
- -7
+ -8.8489
+
+
+
+
+
+
+
+
+ Roll moment due to beta
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ aero/beta-rad
+
+ aero/alpha-rad
+ aero/Re
+
+ 3372885 3710173 5059327 6689612
+ -0.0349 -0.2578 -0.0647 -0.0550 -0.0520
+ 0.3491 -0.6826 -0.1159 -0.1086 -0.1100
+
+
+
+
+
+
+ Roll moment due to roll rate
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ aero/bi2vel
+ velocities/p-aero-rad_sec
+ -0.7313
+
+
+
+
+ Roll moment due to yaw rate
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ aero/bi2vel
+ velocities/r-aero-rad_sec
+
+ aero/alpha-rad
+ aero/Re
+
+ 3372885 3710173 5059327 6689612
+ -0.0349 0.1627 0.0587 0.0533 0.0514
+ 0.3491 4.8174 0.6140 0.6086 0.6068
+
+
+
+
+
+
+ Roll moment due to aileron
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ fcs/left-aileron-pos-rad
+
+ velocities/mach
+
+ 0.0 0.1700
+ 2.0 0.0425
+
+
+
+
+
+
+ Roll moment due to rudder
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ fcs/rudder-pos-rad
+ 0.0100
@@ -732,6 +562,27 @@
+
+
+ Yaw moment due to alpha
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ aero/alpha-rad
+ fcs/gear-no-wow
+
+ aero/beta-rad
+ aero/Re
+
+ 3372885 3710173
+ -0.3491 -1.0000 0.0000
+ 0.3491 1.0000 0.0000
+
+
+
+
+
Yaw moment due to beta
@@ -739,7 +590,27 @@
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
- 0.12
+ 0.0635
+
+
+
+
+ Yaw moment due to roll rate
+
+ aero/qbar-psf
+ metrics/Sw-sqft
+ metrics/bw-ft
+ aero/bi2vel
+ velocities/p-rad_sec
+
+ aero/Re
+
+ 3372885 -2.3531
+ 3710173 -0.2005
+ 5059327 -0.0891
+ 6689612 -0.0510
+
+
@@ -751,7 +622,7 @@
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
- -0.15
+ -0.0474
@@ -762,7 +633,7 @@
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
- -0.1
+ -0.0387
@@ -773,15 +644,14 @@
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
- -0.003
+ -0.0100
-
-
\ No newline at end of file
+