From 8835d0f8a244b6364f1cbe07041952f308aca50f Mon Sep 17 00:00:00 2001 From: murat Date: Thu, 16 Apr 2015 18:20:58 +0200 Subject: [PATCH] JSBSIM model of Eternity A/C is added --- conf/simulator/jsbsim/aircraft/Eternity.xml | 650 ++++++++++++++++++++ 1 file changed, 650 insertions(+) create mode 100644 conf/simulator/jsbsim/aircraft/Eternity.xml diff --git a/conf/simulator/jsbsim/aircraft/Eternity.xml b/conf/simulator/jsbsim/aircraft/Eternity.xml new file mode 100644 index 00000000000..269e7d76863 --- /dev/null +++ b/conf/simulator/jsbsim/aircraft/Eternity.xml @@ -0,0 +1,650 @@ + + + + + + + Murat Bronz + March 2015 + Eternity + + + + + + 0.145 + 1.0 + .145 + .018 + .45 + .012 + .50 + + + 4.0 + 0.0 + 0.0 + + + + 0.0 + 0.0 + 0.0 + + + + 0.0 + 0.0 + 0.0 + + + + + + 0.059 + 0.02465 + 0.07869 + 0.0 + 0.90 + + + 2.0 + 0.0 + 0.0 + + + + + + + + + + + + + + + 27.0 + 0 + -2.0 + + 1.0 + 0.8 + 12 + 1 + + + + -5.0 + 0.0 + 0.0 + + 1.0 + 0.8 + 12 + 1 + + + + 0.0 + 0.0 + -3.0 + + 1.0 + 0.8 + 12 + 1 + + + + + -3.0 + -27.5 + 1.0 + + 1.0 + 0.8 + 12 + 1 + + + + -3.0 + 27.5 + 1.0 + + 1.0 + 0.8 + 12 + 1 + + + + 27.0 + 0.0 + 6.5 + + 1.0 + 0.8 + 12 + 1 + + + + 0.0 + 0.0 + 2.0 + + 1.0 + 0.8 + 12 + 1 + + + + + + + 10.0 + 0 + 3.0 + + + 0.0 + -5 + 0 + + 0 + + + 10.0 + 0 + 3.0 + + + 0.0 + -5.0 + 0.0 + + 1.0 + + + + + + 0.0 + 0.0 + 0.0 + + 0.0001 + 0 + + + + + + + + fcs/elevator-cmd-norm + fcs/pitch-trim-cmd-norm + + -1 + 1 + + fcs/elevator-pos-norm + + + fcs/elevator-pos-norm + fcs/pitch-trim-sum + 0.01745 + + -20 + 15 + + fcs/elevator-pos-rad + + + + + + fcs/aileron-cmd-norm + fcs/roll-trim-cmd-norm + + -1 + 1 + + fcs/aileron-pos-norm + + + fcs/roll-trim-sum + 0.01745 + + -20 + 20 + + fcs/left-aileron-pos-rad + + + fcs/roll-trim-sum + 0.01745 + + -20 + 20 + + fcs/right-aileron-pos-rad + + + + + + fcs/rudder-cmd-norm + fcs/yaw-trim-cmd-norm + + -1 + 1 + + + + fcs/yaw-trim-sum + + -1 + 1 + + + + fcs/yaw-mix + -0.01745 + + -27 + 27 + + fcs/rudder-pos-rad + + + + + + + + fcs/throttle-cmd-norm + 3 + + + + + fcs/rpm-scaled-throttle + + -1 + 1 + + fcs/throttle-pos-norm + + + + + + + + + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.14 -0.06 + -0.0875 0.10 + 0.00 0.50 + 0.14 1.06 + 0.19 1.06 + 0.245 0.8 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.0 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.229 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-deg + + -90.0 1.500 + -6.0 0.03 + 0.00 0.05 + 4.0 0.08 + 8.0 0.105 + 10.0 0.16 + 90.0 1.500 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.0 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.0 + 0.7 0.0 + 1.10 0.0 + 1.80 0.0 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.0 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.0 + + + + + Drag due to sideslip + + aero/qbar-psf + metrics/Sw-sqft + + aero/beta-rad + + -1.57 1.230 + -0.26 0.050 + 0.00 0.000 + 0.26 0.050 + 1.57 1.230 + +
+ + + + + Drag due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-norm + 0.03 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -0.208 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.094 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.4659 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.1345 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.2966 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.00166 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.3215 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-deg + -0.0119 + + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -8.8 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -7 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.0517 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.0914 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.043 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + -0.021 + + + + + + + +