Flight test and simulation results were presented for autonomous aerobatic helicopters. An autonomous aerobatic maneuver was executed on the miniature model helicopter. It was found that a tight yaw rate control by the tail rotor is necessary to counteract large and fast changes in the collective during some maneuvers.
|Original language||English (US)|
|Title of host publication||AIAA/IEEE Digital Avionics Systems Conference - Proceedings|
|State||Published - Jan 1 2002|