Maik Justus schrieb: > > Yes, I get the same here. I think it is related to the collective > position. The rudder function is done by different pitching (cyclic) of > the two rotors. http://en.wikipedia.org/wiki/Tiltrotor .... Yaw <http://en.wikipedia.org/wiki/Yaw_%28flight%29> is controlled by tilting its rotors in opposite directions. ....
Maik, you may already have read this and I am not very familiar with the tiltrotor technology. But *if* they are right then there should at least be an additional tilting-effect to the different cyclic pitching you are using, as I understand. This could be the reason for more responsability - left nacelle little forward tilt, right nacelle little backward tilt, yaw the a/c to the right. But whether this is correct or not - it is wikipedia, so we don't know exactly :-/ But as the wikipedia author goes on writing " Pitch <http://en.wikipedia.org/wiki/Pitch_%28flight%29> is provided through rotor cyclic or nacelle tilt." I think he is pretty well informed about cyclic and common rotor technology. Regards Georg ------------------------------------------------------------------------- This SF.net email is sponsored by: Splunk Inc. Still grepping through log files to find problems? Stop. Now Search log events and configuration files using AJAX and a browser. Download your FREE copy of Splunk now >> http://get.splunk.com/ _______________________________________________ Flightgear-devel mailing list Flightgear-devel@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/flightgear-devel
