David Megginson writes:
>
> Dave Perry writes:
>
> > 2. The adverse aileron yaw is too much at modrate speeds. In fact,
> > since these changes, the wing leveler auto pilot will cause ever
> > increasing aileron oscillations leading to a crash with the
> > c172p.
>
> I'll look into this one. What do you mean by 'moderate' speeds? You
> should be seeing a lot of adverse yaw below 70kt.
The following changes to newauto.hxx allows one to adjust the 'gain'
for this interactively with the autopilot adjuster widget :-)
This widget could be extended to 'tweak' the elevator controls
in a similar manner
// accessors
inline double get_MaxRoll() {
return fgGetFloat( "/autopilot/config/max-roll-deg" );
}
inline double get_RollOut() {
return fgGetFloat( "/autopilot/config/roll-out-deg" );
}
inline double get_MaxAileron() {
return fgGetFloat( "/autopilot/config/max-aileron" );
}
inline double get_RollOutSmooth() {
return fgGetFloat( "/autopilot/config/roll-out-smooth-deg" );
}
inline void set_MaxRoll( double val ) {
fgSetFloat( "/autopilot/config/max-roll-deg", val );
}
inline void set_RollOut( double val ) {
fgSetFloat( "/autopilot/config/roll-out-deg", val );
}
inline void set_MaxAileron( double val ) {
fgSetFloat( "/autopilot/config/max-aileron", val );
}
inline void set_RollOutSmooth( double val ) {
fgSetFloat( "/autopilot/config/roll-out-smooth-deg", val );
}
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