Jim Wilson wrote: > Same as solution for dutch roll effect. No? Not exactly. An autocoordinator moves the rudder to counteract slip angle. A yaw damper moves the rudder to counteract yaw rate, which is the time derivative of slip angle. An aircraft can be held in a slip and a yaw damper won't care, for example. It is even conceivable that an aircraft in a very tight turn (think of an RC plane) could be in coordinated flight but have a non-negligible yaw rate.
Andy _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
