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Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p

This commit is contained in:
daveluff 2006-03-06 21:12:52 +00:00
parent 88da53c862
commit c635f08dc7

View file

@ -219,6 +219,19 @@
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Elevator Position Normalized">
<input>fcs/elevator-pos-deg</input>
<domain>
<min>-28</min>
<max>23</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/elevator-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Roll">
<summer name="Roll Trim Sum">
@ -240,6 +253,19 @@
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Left Aileron Position Normalized">
<input>fcs/left-aileron-pos-deg</input>
<domain>
<min>-20</min>
<max>15</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron Control">
<input>fcs/roll-trim-sum</input>
<gain>-0.01745</gain>
@ -249,6 +275,19 @@
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Right Aileron Position Normalized">
<input>fcs/right-aileron-pos-deg</input>
<domain>
<min>-15</min>
<max>20</max>
</domain>
<range>
<min>1</min>
<max>-1</max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Yaw">
<summer name="Yaw Trim Sum">
@ -269,6 +308,19 @@
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder Position Normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
<min>-16</min>
<max>16</max>
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Flaps">
<kinematic name="Flaps Control">
@ -293,6 +345,19 @@
</traverse>
<output>fcs/flap-pos-deg</output>
</kinematic>
<aerosurface_scale name="Flaps Position Normalized">
<input>fcs/flap-pos-deg</input>
<domain>
<min>0</min>
<max>30</max>
</domain>
<range>
<min>0</min>
<max>1</max>
</range>
<output>fcs/flap-pos-norm</output>
</aerosurface_scale>
</channel>
</flight_control>
<aerodynamics>