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F-15 coefficients for yawing moment due to rudder deflection elevator #12

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Zaretto opened this issue Dec 19, 2015 · 0 comments
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@Zaretto
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Zaretto commented Dec 19, 2015

CNDRDe should be a function of (alpha,beta,elevator) - however this would require a 4d table.

Need to fix this, either using the multi-dimensional method that Jon Berndt wrote about, or to separate these out into separate lookup tables that can be combined.

ref: https://github.com/Zaretto/fg-aircraft/blob/master/aircraft/f-14b/F14AeroPlot/F14AeroPlot/F15Aero.cs#L963

Zaretto added a commit that referenced this issue Mar 19, 2016
The bindings on the throttle were correct; in that the selector needs to be changed and a weapons system refresh requested. Fix this by adding a listener to the property to always do this rather than relying on inline code.
Zaretto added a commit that referenced this issue May 1, 2024
added elevator-pos to CMNDRDr (YAWING MOMENT DUE TO RUDDER DEFLECTIION) as per the Baumann aero model.
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