diff --git a/A319-100-CFM.xml b/A319-100-CFM.xml index 4e70c01a..2a887500 100644 --- a/A319-100-CFM.xml +++ b/A319-100-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A319-100-IAE.xml b/A319-100-IAE.xml index 80707b55..8e54cc0c 100644 --- a/A319-100-IAE.xml +++ b/A319-100-IAE.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A320-200-CFM.xml b/A320-200-CFM.xml index a24fc369..a84a9ba0 100644 --- a/A320-200-CFM.xml +++ b/A320-200-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A320-200-IAE.xml b/A320-200-IAE.xml index ab20ec08..371cd4d0 100644 --- a/A320-200-IAE.xml +++ b/A320-200-IAE.xml @@ -580,390 +580,21 @@ YAW MOI_________3950000______23089847_______24848934 + + - - - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A320-main.xml b/A320-main.xml index 525fce74..4ce7b8e9 100644 --- a/A320-main.xml +++ b/A320-main.xml @@ -79,16 +79,19 @@ Aircraft/A320Family/Systems/fmgc-b.xml - + + Aircraft/A320Family/Systems/fmgc-roll-yaw.xml + + + Aircraft/A320Family/Systems/fmgc-pitch.xml + + Aircraft/A320Family/Systems/custom-autothrust.xml - + Aircraft/A320Family/Systems/libraries.xml - - Aircraft/A320Family/Systems/fmgc-c.xml - - + Systems/fl2070_sound.xml diff --git a/A321-200-CFM.xml b/A321-200-CFM.xml index d8dbab47..324e2a2d 100644 --- a/A321-200-CFM.xml +++ b/A321-200-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A321-200-IAE.xml b/A321-200-IAE.xml index d72b47ee..3b84756d 100644 --- a/A321-200-IAE.xml +++ b/A321-200-IAE.xml @@ -579,391 +579,22 @@ YAW MOI_________3950000______23089847_______24848934 - + - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - 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 - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/AircraftConfig/acconfig.nas b/AircraftConfig/acconfig.nas index 5fceaa20..0097d780 100644 --- a/AircraftConfig/acconfig.nas +++ b/AircraftConfig/acconfig.nas @@ -349,7 +349,7 @@ var takeoff = func { setprop("/controls/flight/flap-pos", 2); setprop("/controls/flight/flap-txt", "1+F"); libraries.flaptimer.start(); - setprop("/controls/flight/elevator-trim", -0.15); + setprop("/controls/flight/elevator-trim", -0.07); } }); } diff --git a/Systems/a319-aerodynamics.xml b/Systems/a319-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a319-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + 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 + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/a320-aerodynamics.xml b/Systems/a320-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a320-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + 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 + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/a321-aerodynamics.xml b/Systems/a321-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a321-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + 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 + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/fadec-cfm.xml b/Systems/fadec-cfm.xml index 5057b01d..add9e078 100644 --- a/Systems/fadec-cfm.xml +++ b/Systems/fadec-cfm.xml @@ -1,5 +1,8 @@ + + + @@ -436,7 +439,7 @@ /engines/engine[0]/n1 - 23 + 22 @@ -469,7 +472,7 @@ /engines/engine[1]/n1 - 23 + 22 diff --git a/Systems/fadec-iae.xml b/Systems/fadec-iae.xml index 1a72e389..c0d91476 100644 --- a/Systems/fadec-iae.xml +++ b/Systems/fadec-iae.xml @@ -1,5 +1,8 @@ + + + @@ -702,7 +705,7 @@ /engines/engine[0]/n1 - 23 + 22 @@ -735,7 +738,7 @@ /engines/engine[1]/n1 - 23 + 22 @@ -755,4 +758,4 @@ /engines/engine[1]/egt-actual - + \ No newline at end of file diff --git a/Systems/fmgc-b.xml b/Systems/fmgc-b.xml index f6b7d7a8..e0cfbaf9 100644 --- a/Systems/fmgc-b.xml +++ b/Systems/fmgc-b.xml @@ -72,9 +72,91 @@ - + + + FMGC MNG SPD + gain + 1 + 0.05 + + + + + /instrumentation/altimeter/indicated-altitude-ft + 10000286 + 42000249 +
+ + /FMGC/internal/cost-index + 01.0 + 1201.1 +
+ + + + /FMGC/internal/mng-alt-spd + + + + FMGC MNG MACH + gain + 1 + 0.05 + + + + + /instrumentation/altimeter/indicated-altitude-ft + 260000.705 + 420000.815 +
+ + /FMGC/internal/cost-index + 00.97 + 1201.03 +
+ + + + /FMGC/internal/mng-alt-mach + + + + FMGC Target IAS PFD + gain + 1 + 0.1 + + + + /it-autoflight/input/kts-mach + 0 + + + /it-autoflight/input/spd-kts + + + + + /it-autoflight/input/kts-mach + 1 + + + + +
+ /instrumentation/airspeed-indicator/indicated-speed-kt + /instrumentation/airspeed-indicator/indicated-mach +
+ /it-autoflight/input/spd-mach + + + + /FMGC/internal/target-ias-pfd + + KTS INPUT FILTER false @@ -389,1097 +471,6 @@ -1500 0 - - - - - - - ROLL CONTROLLER: HDG/LNAV - false - - - - - - /it-autoflight/output/lat - 0 - - - /it-autoflight/output/lat - 1 - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - - - /it-autoflight/internal/heading-error-deg - - /it-autoflight/config/cmd/roll-scale - - - - 0 - - - /it-autoflight/internal/target-roll-deg - - - - /it-autoflight/config/cmd/roll-kp - - 0.0 - - - - /it-autoflight/output/lat - 1 - - - /it-autoflight/input/bank-limit - -1 - - - - - /it-autoflight/output/lat - 1 - - - -25 - - - - - /it-autoflight/output/lat - 1 - - - /it-autoflight/input/bank-limit - - - - - /it-autoflight/output/lat - 1 - - - 25 - - - - - - VORLOC TRK - false - - - - - /it-autoflight/output/lat - 2 - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - - - - - /it-autoflight/settings/use-backcourse - 0 - - - /it-autoflight/internal/nav-heading-error-deg - - - - - /it-autoflight/settings/use-backcourse - 1 - - - /it-autoflight/internal/nav-bc-heading-error-deg - - - 0.0 - - - /it-autoflight/internal/target-roll-deg - - - - /it-autoflight/config/cmd/vorloc - - 1.0 - 0.1 - 0.0 - 10.0 - 0.00001 - -25 - 25 - - - - - ROLL DEG SYNC - false - gain - 1 - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - /orientation/roll-deg - /it-autoflight/internal/target-roll-deg - -25 - 25 - - - - IT-CONTROLLER: TARGET ROLL CMD - false - true - output - - /it-autoflight/internal/target-roll-deg - - /it-autoflight/internal/target-roll - noise-spike - 6 - - - - IT-CONTROLLER: ROLL - false - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - /orientation/roll-deg - - - - - - /it-autoflight/output/lat - 4 - - - /it-autoflight/output/lat - 5 - - - - /it-autoflight/internal/target-roll - - - - - - /it-autoflight/output/lat - 4 - - - /it-autoflight/output/lat - 5 - - - - 0 - - - /it-autoflight/internal/aileron-cmd - - - - - - /it-autoflight/output/lat - 2 - - - /it-autoflight/config/roll/kp - - - - - /it-autoflight/output/lat - 2 - - - /it-autoflight/config/roll/kp-vloc - - 1.0 - 0.1 - 0.0 - - /it-autoflight/config/roll/ti - - - /it-autoflight/config/roll/td - - - /it-autoflight/config/roll/umin - - - /it-autoflight/config/roll/umax - - - - - - IT-CONTROLLER: ROLL CMD - false - true - output - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - /it-autoflight/internal/aileron-cmd - - /controls/flight/aileron - noise-spike - 0.5 - - - - - - - - ALTITUDE CAPTURE/HOLD - false - gain - - /it-autoflight/internal/altitude-5-sec-ahead - - - /it-autoflight/internal/alt - - -8 - - /it-autoflight/internal/target-fpm - - - /it-autoflight/internal/min-vs - - - /it-autoflight/internal/max-vs - - - - - FPA HOLD - false - - - - - /it-autoflight/output/vert - 5 - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - - - /it-autoflight/internal/fpa - - - /it-autoflight/input/fpa - - - /it-autoflight/internal/target-pitch-deg - - - - /it-autoflight/config/cmd/fpa - - 1.0 - 0.1 - 0.0 - 1.0 - 0.00001 - - -10 - - - 30 - - - - - - FLCH SPEED BY PITCH - false - - - - - /it-autoflight/output/vert - 4 - - - /it-autoflight/output/vert - 7 - - - - - - - - /it-autoflight/input/kts-mach - 0 - - - /it-autoflight/internal/lookahead-15-sec-airspeed-kt - - - - - /it-autoflight/input/kts-mach - 1 - - - /it-autoflight/internal/lookahead-15-sec-mach - 500.0 - - - - - /it-autoflight/input/kts-mach - 0 - - - /it-autoflight/internal/flch-kts - - - - - /it-autoflight/input/kts-mach - 1 - - - /it-autoflight/internal/flch-mach - 500.0 - - - /it-autoflight/internal/target-fpm-b - - - - - - /it-autoflight/output/vert - 4 - - - -50 - - - - - /it-autoflight/output/vert - 7 - - - -60 - - 1.0 - 0.1 - 0.0 - 2.5 - 0.001 - - - - /it-autoflight/output/thr-mode - 2 - - - 150 - - - - - /it-autoflight/output/thr-mode - 1 - - - -6000 - - - - - - /it-autoflight/output/thr-mode - 2 - - - - /gear/gear[1]/wow - 0 - - - /gear/gear[2]/wow - 0 - - - - - 10000 - - - - - - /it-autoflight/output/thr-mode - 2 - - - - /gear/gear[1]/wow - 1 - - - /gear/gear[2]/wow - 1 - - - - - 1000 - - - - - /it-autoflight/output/thr-mode - 1 - - - -150 - - - - - - AUTOLAND FPM - gain - 1 - 0.05 - - - - /position/gear-agl-ft - 100-600 - 50-500 - 40-400 - 30-300 - 20-200 - 10-150 - 5-100 -
- - - /it-autoflight/internal/target-fpm-c - - - - FPM HOLD - false - - - - - - /it-autoflight/output/vert - 0 - - - /it-autoflight/output/vert - 1 - - - /it-autoflight/output/vert - 2 - - - /it-autoflight/output/vert - 4 - - - /it-autoflight/output/vert - 6 - - - /it-autoflight/output/vert - 7 - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - - - /it-autoflight/internal/vert-speed-fpm - 0.16667 - - - - - /it-autoflight/output/vert - 0 - - - /it-autoflight/internal/target-fpm - 0.16667 - - - - - /it-autoflight/output/vert - 1 - - - /it-autoflight/internal/vs - 0.16667 - - - - - - /it-autoflight/output/vert - 4 - - - /it-autoflight/output/vert - 7 - - - - /it-autoflight/internal/target-fpm-b - 0.16667 - - - - - /it-autoflight/output/vert - 6 - - - /it-autoflight/internal/target-fpm-c - 0.16667 - - - - - /it-autoflight/output/vert - 2 - - - /it-autoflight/internal/nav1-rate-of-climb-fpm - 0.16667 - - - /it-autoflight/internal/target-pitch-deg - - - - - - /it-autoflight/output/vert - 6 - - - /it-autoflight/config/cmd/vs - - - - - /it-autoflight/output/vert - 6 - - - /it-autoflight/config/autoland/kp-pitch - - 7.0 - 0.0001 - - - - /it-autoflight/output/vert - 6 - - - -10 - - - - - /it-autoflight/output/vert - 6 - - - 0 - - - - - - /gear/gear[1]/wow - 0 - - - /gear/gear[2]/wow - 0 - - - - 30 - - - - - - /gear/gear[1]/wow - 1 - - - /gear/gear[2]/wow - 1 - - - - 10 - - - - - - PITCH DEG SYNC - false - gain - 1 - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - /it-autoflight/output/fd1 - 1 - - - /it-autoflight/output/fd2 - 1 - - - - - /orientation/pitch-deg - /it-autoflight/internal/target-pitch-deg - -15 - 30 - - - - IT-CONTROLLER: PITCH - false - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - /orientation/pitch-deg - - - /it-autoflight/internal/target-pitch-deg - - - /it-autoflight/internal/elevator-cmd - - - - /it-autoflight/config/pitch/kp - - 1.0 - 0.1 - 0.0 - - /it-autoflight/config/pitch/ti - - - /it-autoflight/config/pitch/td - - - /it-autoflight/config/pitch/umin - - - /it-autoflight/config/pitch/umax - - - - - - IT-CONTROLLER: PITCH CMD - false - true - output - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - /it-autoflight/internal/elevator-cmd - - /controls/flight/elevator - noise-spike - 0.4 - - - - - - - - RUDDER VORLOC TRK - false - - - - /it-autoflight/output/lat - 4 - - - - - /it-autoflight/internal/nav-heading-error-deg - - - 0 - - /it-autoflight/internal/rudder-cmd - - - /it-autoflight/config/autoland/kp-rudder - - 0 - - -0.25 - 0.25 - - - - IT-CONTROLLER: RUDDER CMD - false - true - output - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - - - /it-autoflight/output/lat - 4 - - - 0 - - - - - /it-autoflight/output/lat - 4 - - - /it-autoflight/internal/rudder-cmd - - /controls/flight/rudder - noise-spike - 0.20 - - - - - - - - AP PITCH HELPER PLUS - false - - - - - /it-autoflight/internal/elevator-cmd - 0.01 - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - - 0 - - - 1 - - - /it-autoflight/internal/elevator-trim-cmd - - - 0.08 - 1.0 - 0.1 - 0.0 - 10 - 0.00001 - -1.00 - 1.00 - - - - - AP PITCH HELPER MINUS - false - - - - - /it-autoflight/internal/elevator-cmd - -0.01 - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - - - 0 - - - 1 - - - /it-autoflight/internal/elevator-trim-cmd - - - -0.08 - 1.0 - 0.1 - 0.0 - 10 - 0.00001 - -1.00 - 1.00 - - - - - IT-CONTROLLER: PITCH TRIM CMD - false - true - output - - - - - - /it-autoflight/output/ap1 - 1 - - - /it-autoflight/output/ap2 - 1 - - - - - /it-autoflight/internal/elevator-cmd - 0.01 - - - /it-autoflight/internal/elevator-cmd - -0.01 - - - - - - - /it-autoflight/internal/elevator-trim-cmd - - /controls/flight/elevator-trim - noise-spike - 0.01 - diff --git a/Systems/fmgc-c.xml b/Systems/fmgc-c.xml deleted file mode 100644 index 236fa249..00000000 --- a/Systems/fmgc-c.xml +++ /dev/null @@ -1,87 +0,0 @@ - - - - - - FMGC MNG SPD - gain - 1 - 0.05 - - - - - /instrumentation/altimeter/indicated-altitude-ft - 10000286 - 42000249 -
- - /FMGC/internal/cost-index - 01.0 - 1201.1 -
- - - - /FMGC/internal/mng-alt-spd - - - - FMGC MNG MACH - gain - 1 - 0.05 - - - - - /instrumentation/altimeter/indicated-altitude-ft - 260000.705 - 420000.815 -
- - /FMGC/internal/cost-index - 00.97 - 1201.03 -
- - - - /FMGC/internal/mng-alt-mach - - - - FMGC Target IAS PFD - gain - 1 - 0.1 - - - - /it-autoflight/input/kts-mach - 0 - - - /it-autoflight/input/spd-kts - - - - - /it-autoflight/input/kts-mach - 1 - - - - -
- /instrumentation/airspeed-indicator/indicated-speed-kt - /instrumentation/airspeed-indicator/indicated-mach -
- /it-autoflight/input/spd-mach - - - - /FMGC/internal/target-ias-pfd - - - diff --git a/Systems/fmgc-pitch.xml b/Systems/fmgc-pitch.xml new file mode 100644 index 00000000..92c17da4 --- /dev/null +++ b/Systems/fmgc-pitch.xml @@ -0,0 +1,694 @@ + + + + + + + + + + + + ALTITUDE CAPTURE/HOLD + false + gain + + /it-autoflight/internal/altitude-5-sec-ahead + + + /it-autoflight/internal/alt + + -8 + + /it-autoflight/internal/target-fpm + + + /it-autoflight/internal/min-vs + + + /it-autoflight/internal/max-vs + + + + + FPA HOLD + false + + + + + /it-autoflight/output/vert + 5 + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + + + /it-autoflight/internal/fpa + + + /it-autoflight/input/fpa + + + /it-autoflight/internal/target-pitch-deg + + + + /it-autoflight/config/cmd/fpa + + 1.0 + 0.1 + 0.0 + 1.0 + 0.00001 + + -10 + + + 30 + + + + + + FLCH SPEED BY PITCH + false + + + + + /it-autoflight/output/vert + 4 + + + /it-autoflight/output/vert + 7 + + + + + + + + /it-autoflight/input/kts-mach + 0 + + + /it-autoflight/internal/lookahead-15-sec-airspeed-kt + + + + + /it-autoflight/input/kts-mach + 1 + + + /it-autoflight/internal/lookahead-15-sec-mach + 500.0 + + + + + /it-autoflight/input/kts-mach + 0 + + + /it-autoflight/internal/flch-kts + + + + + /it-autoflight/input/kts-mach + 1 + + + /it-autoflight/internal/flch-mach + 500.0 + + + /it-autoflight/internal/target-fpm-b + + + + + + /it-autoflight/output/vert + 4 + + + -50 + + + + + /it-autoflight/output/vert + 7 + + + -60 + + 1.0 + 0.1 + 0.0 + 2.5 + 0.001 + + + + /it-autoflight/output/thr-mode + 2 + + + 150 + + + + + /it-autoflight/output/thr-mode + 1 + + + -6000 + + + + + + /it-autoflight/output/thr-mode + 2 + + + + /gear/gear[1]/wow + 0 + + + /gear/gear[2]/wow + 0 + + + + + 10000 + + + + + + /it-autoflight/output/thr-mode + 2 + + + + /gear/gear[1]/wow + 1 + + + /gear/gear[2]/wow + 1 + + + + + 1000 + + + + + /it-autoflight/output/thr-mode + 1 + + + -150 + + + + + + AUTOLAND FPM + gain + 1 + 0.05 + + + + /position/gear-agl-ft + 100-600 + 50-500 + 40-400 + 30-300 + 20-200 + 10-150 + 5-100 +
+ + + /it-autoflight/internal/target-fpm-c + + + + FPM HOLD + false + + + + + + /it-autoflight/output/vert + 0 + + + /it-autoflight/output/vert + 1 + + + /it-autoflight/output/vert + 2 + + + /it-autoflight/output/vert + 4 + + + /it-autoflight/output/vert + 6 + + + /it-autoflight/output/vert + 7 + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + + + /it-autoflight/internal/vert-speed-fpm + 0.16667 + + + + + /it-autoflight/output/vert + 0 + + + /it-autoflight/internal/target-fpm + 0.16667 + + + + + /it-autoflight/output/vert + 1 + + + /it-autoflight/internal/vs + 0.16667 + + + + + + /it-autoflight/output/vert + 4 + + + /it-autoflight/output/vert + 7 + + + + /it-autoflight/internal/target-fpm-b + 0.16667 + + + + + /it-autoflight/output/vert + 6 + + + /it-autoflight/internal/target-fpm-c + 0.16667 + + + + + /it-autoflight/output/vert + 2 + + + /it-autoflight/internal/nav1-rate-of-climb-fpm + 0.16667 + + + /it-autoflight/internal/target-pitch-deg + + + + + + /it-autoflight/output/vert + 6 + + + /it-autoflight/config/cmd/vs + + + + + /it-autoflight/output/vert + 6 + + + /it-autoflight/config/autoland/kp-pitch + + 7.0 + 0.0001 + + + + /it-autoflight/output/vert + 6 + + + -10 + + + + + /it-autoflight/output/vert + 6 + + + 0 + + + + + + /gear/gear[1]/wow + 0 + + + /gear/gear[2]/wow + 0 + + + + 30 + + + + + + /gear/gear[1]/wow + 1 + + + /gear/gear[2]/wow + 1 + + + + 10 + + + + + + PITCH DEG SYNC + false + gain + 1 + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + /orientation/pitch-deg + /it-autoflight/internal/target-pitch-deg + -15 + 30 + + + + IT-CONTROLLER: PITCH + false + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + /orientation/pitch-deg + + + /it-autoflight/internal/target-pitch-deg + + + /it-autoflight/internal/elevator-cmd + + + + /it-autoflight/config/pitch/kp + + 1.0 + 0.1 + 0.0 + + /it-autoflight/config/pitch/ti + + + /it-autoflight/config/pitch/td + + + /it-autoflight/config/pitch/umin + + + /it-autoflight/config/pitch/umax + + + + + + IT-CONTROLLER: PITCH CMD + false + true + output + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + /it-autoflight/internal/elevator-cmd + + /controls/flight/elevator + noise-spike + 0.4 + + + + + + + + AP PITCH HELPER PLUS + false + + + + + /it-autoflight/internal/elevator-cmd + 0.01 + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + + 0 + + + 1 + + + /it-autoflight/internal/elevator-trim-cmd + + + 0.08 + 1.0 + 0.1 + 0.0 + 10 + 0.00001 + -1.00 + 1.00 + + + + + AP PITCH HELPER MINUS + false + + + + + /it-autoflight/internal/elevator-cmd + -0.01 + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + + 0 + + + 1 + + + /it-autoflight/internal/elevator-trim-cmd + + + -0.08 + 1.0 + 0.1 + 0.0 + 10 + 0.00001 + -1.00 + 1.00 + + + + + IT-CONTROLLER: PITCH TRIM CMD + false + true + output + + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + /it-autoflight/internal/elevator-cmd + 0.01 + + + /it-autoflight/internal/elevator-cmd + -0.01 + + + + + + + /it-autoflight/internal/elevator-trim-cmd + + /controls/flight/elevator-trim + noise-spike + 0.01 + + + diff --git a/Systems/fmgc-roll-yaw.xml b/Systems/fmgc-roll-yaw.xml new file mode 100644 index 00000000..fba0f363 --- /dev/null +++ b/Systems/fmgc-roll-yaw.xml @@ -0,0 +1,411 @@ + + + + + + + + + + + + ROLL CONTROLLER: HDG/LNAV + false + + + + + + /it-autoflight/output/lat + 0 + + + /it-autoflight/output/lat + 1 + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + + + /it-autoflight/internal/heading-error-deg + + /it-autoflight/config/cmd/roll-scale + + + + 0 + + + /it-autoflight/internal/target-roll-deg + + + + /it-autoflight/config/cmd/roll-kp + + 0.0 + + + + /it-autoflight/output/lat + 1 + + + /it-autoflight/input/bank-limit + -1 + + + + + /it-autoflight/output/lat + 1 + + + -25 + + + + + /it-autoflight/output/lat + 1 + + + /it-autoflight/input/bank-limit + + + + + /it-autoflight/output/lat + 1 + + + 25 + + + + + + VORLOC TRK + false + + + + + /it-autoflight/output/lat + 2 + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + + + + + /it-autoflight/settings/use-backcourse + 0 + + + /it-autoflight/internal/nav-heading-error-deg + + + + + /it-autoflight/settings/use-backcourse + 1 + + + /it-autoflight/internal/nav-bc-heading-error-deg + + + 0.0 + + + /it-autoflight/internal/target-roll-deg + + + + /it-autoflight/config/cmd/vorloc + + 1.0 + 0.1 + 0.0 + 10.0 + 0.00001 + -25 + 25 + + + + + ROLL DEG SYNC + false + gain + 1 + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + /it-autoflight/output/fd1 + 1 + + + /it-autoflight/output/fd2 + 1 + + + + + /orientation/roll-deg + /it-autoflight/internal/target-roll-deg + -25 + 25 + + + + IT-CONTROLLER: TARGET ROLL CMD + false + true + output + + /it-autoflight/internal/target-roll-deg + + /it-autoflight/internal/target-roll + noise-spike + 6 + + + + IT-CONTROLLER: ROLL + false + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + /orientation/roll-deg + + + + + + /it-autoflight/output/lat + 4 + + + /it-autoflight/output/lat + 5 + + + + /it-autoflight/internal/target-roll + + + + + + /it-autoflight/output/lat + 4 + + + /it-autoflight/output/lat + 5 + + + + 0 + + + /it-autoflight/internal/aileron-cmd + + + + + + /it-autoflight/output/lat + 2 + + + /it-autoflight/config/roll/kp + + + + + /it-autoflight/output/lat + 2 + + + /it-autoflight/config/roll/kp-vloc + + 1.0 + 0.1 + 0.0 + + /it-autoflight/config/roll/ti + + + /it-autoflight/config/roll/td + + + /it-autoflight/config/roll/umin + + + /it-autoflight/config/roll/umax + + + + + + IT-CONTROLLER: ROLL CMD + false + true + output + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + /it-autoflight/internal/aileron-cmd + + /controls/flight/aileron + noise-spike + 0.5 + + + + + + + + RUDDER VORLOC TRK + false + + + + /it-autoflight/output/lat + 4 + + + + + /it-autoflight/internal/nav-heading-error-deg + + + 0 + + /it-autoflight/internal/rudder-cmd + + + /it-autoflight/config/autoland/kp-rudder + + 0 + + -0.25 + 0.25 + + + + IT-CONTROLLER: RUDDER CMD + false + true + output + + + + + /it-autoflight/output/ap1 + 1 + + + /it-autoflight/output/ap2 + 1 + + + + + + + + /it-autoflight/output/lat + 4 + + + 0 + + + + + /it-autoflight/output/lat + 4 + + + /it-autoflight/internal/rudder-cmd + + /controls/flight/rudder + noise-spike + 0.20 + + + diff --git a/Systems/it-fbw.xml b/Systems/it-fbw.xml index 0f8cd88d..a695f473 100644 --- a/Systems/it-fbw.xml +++ b/Systems/it-fbw.xml @@ -1,4 +1,4 @@ - + /it-fbw/law @@ -100,19 +100,19 @@ /controls/flight/elevator-input - -1.0 0.0750 - -0.7 0.0530 - -0.5 0.0220 - -0.3 0.0110 - -0.15 0.0040 + -1.0 0.0755 + -0.7 0.0535 + -0.5 0.0225 + -0.3 0.0115 + -0.15 0.0045 -0.05 0.0007 0.00 0.0000 0.05 -0.0007 - 0.15 -0.0040 - 0.3 -0.0110 - 0.5 -0.0220 - 0.7 -0.0530 - 1.0 -0.0750 + 0.15 -0.0045 + 0.3 -0.0115 + 0.5 -0.0225 + 0.7 -0.0535 + 1.0 -0.0755