> >> The SenecaII wing rock with light turbulence appears to result from a
> >> very exaggerated adverse aileron yaw.  So I did the same experiment
with
> >> the c172p and pa28-140 which both use the kap140.  With the default
> >> turbulence, the c172p oscillates so bad that you cannot complete the
> >> approach with the LOC needle going full stop to full stop near the
> >> runway.  The pa28-161 (also yasim) is as solid as a rock all the way
> >> down the glide slope with light to moderate turbulence.


Another thing I'd like to see is a test from steady state that reproduces
the worst of the problem with no turbulence. That way I can set up a similar
test in JSBSim by itself and script a set of maneuvers that duplicates the
problem.

Jon



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