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Jun 11, 2018 at 17:33 comment added Walker Enstrom helicopters use the Universal (Hookes) Joint design. Control feedback not as well mitigated with this design.
Jun 8, 2018 at 6:28 comment added Zeus @user31222, theoretically everything is feasible, but why? Just think: Stewart platform is a 6-DoF machine, while the swashplate is 3-DoF (plus each needs to pass continuous rotation). It's an order of magnitude more complexity, and what for?
Jun 7, 2018 at 15:05 vote accept user31222
Jun 8, 2018 at 8:26
Jun 7, 2018 at 15:03 comment added user31222 I have read both the wikipedia article and the LADDM paper. I wanted to know if it would be feasible to use this mechanism in a helicopter to tilt the rotor head and if not why?
Jun 7, 2018 at 13:39 history answered CrossRoads CC BY-SA 4.0