A32X: FCS, and Aero Improvements
This commit is contained in:
Joshua Davidson
parent
7596cd0f13
commit
032017a6aa
6 changed files with 85 additions and 106 deletions
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@ -262,7 +262,7 @@
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<value>-0.95</value>
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<value>-0.91</value>
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</product>
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</function>
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@ -278,14 +278,14 @@
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</product>
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</function>
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<function name="aero/moment/Roll_aileron">
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<description>Roll moment due to aileron</description>
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<function name="aero/moment/Roll_control">
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<description>Roll moment due to roll control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0.20</value>
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<property>fcs/roll-pos-rad</property>
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<value>0.11</value>
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</product>
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</function>
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@ -315,19 +315,19 @@
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</product>
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</function>
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<function name="aero/moment/Pitch_elevator">
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<description>Pitch moment due to elevator</description>
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<function name="aero/moment/Pitch_control">
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<description>Pitch moment due to pitch control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>fcs/elevator-pos-rad</property>
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<property>fcs/pitch-pos-rad</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -2.200
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0.2 -2.100
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2.0 -0.900
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0.0 -1.750
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0.2 -1.650
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2.0 -0.700
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</tableData>
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</table>
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</product>
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@ -341,7 +341,7 @@
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>velocities/q-aero-rad_sec</property>
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<value>-140</value>
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<value>-136</value>
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</product>
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</function>
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@ -262,7 +262,7 @@
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<value>-0.95</value>
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<value>-0.91</value>
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</product>
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</function>
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@ -278,14 +278,14 @@
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</product>
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</function>
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<function name="aero/moment/Roll_aileron">
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<description>Roll moment due to aileron</description>
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<function name="aero/moment/Roll_control">
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<description>Roll moment due to roll control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0.20</value>
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<property>fcs/roll-pos-rad</property>
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<value>0.11</value>
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</product>
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</function>
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@ -315,19 +315,19 @@
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</product>
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</function>
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<function name="aero/moment/Pitch_elevator">
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<description>Pitch moment due to elevator</description>
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<function name="aero/moment/Pitch_control">
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<description>Pitch moment due to pitch control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>fcs/elevator-pos-rad</property>
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<property>fcs/pitch-pos-rad</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -2.200
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0.2 -2.100
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2.0 -0.900
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0.0 -1.750
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0.2 -1.650
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2.0 -0.700
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</tableData>
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</table>
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</product>
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@ -341,7 +341,7 @@
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>velocities/q-aero-rad_sec</property>
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<value>-140</value>
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<value>-136</value>
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</product>
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</function>
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@ -262,7 +262,7 @@
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<value>-0.95</value>
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<value>-0.91</value>
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</product>
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</function>
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@ -278,14 +278,14 @@
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</product>
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</function>
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<function name="aero/moment/Roll_aileron">
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<description>Roll moment due to aileron</description>
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<function name="aero/moment/Roll_control">
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<description>Roll moment due to roll control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0.20</value>
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<property>fcs/roll-pos-rad</property>
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<value>0.11</value>
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</product>
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</function>
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@ -315,19 +315,19 @@
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</product>
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</function>
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<function name="aero/moment/Pitch_elevator">
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<description>Pitch moment due to elevator</description>
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<function name="aero/moment/Pitch_control">
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<description>Pitch moment due to pitch control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>fcs/elevator-pos-rad</property>
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<property>fcs/pitch-pos-rad</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -2.200
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0.2 -2.100
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2.0 -0.900
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0.0 -1.750
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0.2 -1.650
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2.0 -0.700
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</tableData>
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</table>
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</product>
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@ -341,7 +341,7 @@
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>velocities/q-aero-rad_sec</property>
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<value>-140</value>
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<value>-136</value>
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</product>
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</function>
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@ -262,7 +262,7 @@
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<property>metrics/bw-ft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
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<value>-0.95</value>
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<value>-0.91</value>
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</product>
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</function>
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@ -278,14 +278,14 @@
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</product>
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</function>
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<function name="aero/moment/Roll_aileron">
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<description>Roll moment due to aileron</description>
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<function name="aero/moment/Roll_control">
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<description>Roll moment due to roll control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>0.20</value>
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<property>fcs/roll-pos-rad</property>
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<value>0.11</value>
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</product>
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</function>
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@ -315,19 +315,19 @@
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</product>
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</function>
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<function name="aero/moment/Pitch_elevator">
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<description>Pitch moment due to elevator</description>
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<function name="aero/moment/Pitch_control">
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<description>Pitch moment due to pitch control</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>metrics/cbarw-ft</property>
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<property>fcs/elevator-pos-rad</property>
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<property>fcs/pitch-pos-rad</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.0 -2.200
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0.2 -2.100
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2.0 -0.900
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0.0 -1.750
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0.2 -1.650
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2.0 -0.700
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</tableData>
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</table>
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</product>
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@ -341,7 +341,7 @@
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<property>metrics/cbarw-ft</property>
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<property>aero/ci2vel</property>
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<property>velocities/q-aero-rad_sec</property>
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<value>-140</value>
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<value>-136</value>
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</product>
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</function>
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@ -7,38 +7,6 @@
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-->
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<system name="A3XX: FCS">
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<channel name="Pitch">
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<summer name="Pitch Trim Sum">
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<input>/controls/flight/elevator-sum</input>
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<input>/controls/flight/elevator-trim</input>
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<clipto>
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<min>-1</min>
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<max>1</max>
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</clipto>
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</summer>
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<aerosurface_scale name="Elevator Control">
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<input>fcs/pitch-trim-sum</input>
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<gain>0.02</gain>
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<range>
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<min>-20</min>
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<max>20</max>
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</range>
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<output>fcs/elevator-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Elevator Position Normalizer">
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<input>fcs/pitch-trim-sum</input>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/elevator-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Roll">
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@ -51,50 +19,61 @@
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</clipto>
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</summer>
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<aerosurface_scale name="Left Aileron Control">
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<aerosurface_scale name="Roll Control">
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<input>fcs/roll-trim-sum</input>
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<gain>0.02</gain>
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<range>
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<min>-15</min>
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<max>15</max>
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<min>-0.523599</min>
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<max>0.523599</max>
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</range>
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<output>fcs/left-aileron-pos-rad</output>
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<output>fcs/roll-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Right Aileron Control">
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<input>-fcs/roll-trim-sum</input>
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<gain>0.02</gain>
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<range>
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<min>-15</min>
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<max>15</max>
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</range>
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<output>fcs/right-aileron-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Left Aileron position normalized">
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<input>fcs/left-aileron-pos-deg</input>
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<aerosurface_scale name="Roll Control Normalized">
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<input>fcs/roll-pos-rad</input>
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<domain>
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<min>-15</min>
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<max>15</max>
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<min>-0.523599</min>
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<max>0.523599</max>
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</domain>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/left-aileron-pos-norm</output>
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<output>fcs/roll-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Pitch">
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<summer name="Pitch Trim Sum">
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<input>/controls/flight/elevator-sum</input>
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<input>/controls/flight/elevator-trim</input>
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<clipto>
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<min>-1</min>
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<max>1</max>
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</clipto>
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</summer>
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<aerosurface_scale name="Right Aileron position normalized">
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<input>fcs/right-aileron-pos-deg</input>
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<aerosurface_scale name="Pitch Control">
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<input>fcs/pitch-trim-sum</input>
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<range>
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<min>-0.523599</min>
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<max>0.523599</max>
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</range>
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<output>fcs/pitch-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Pitch Control Normalized">
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<input>fcs/pitch-trim-sum</input>
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<domain>
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<min>-15</min>
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<max>15</max>
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<min>-0.523599</min>
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<max>0.523599</max>
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</domain>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/right-aileron-pos-norm</output>
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<output>fcs/pitch-pos-norm</output>
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</aerosurface_scale>
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</channel>
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@ -1 +1 @@
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2031
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2100
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Reference in a new issue