Abstract
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 |
| Volume | 2 |
| State | Published - Jan 1 2002 |
| Event | Air Traffic Management for Commercial and Military Systems - Irvine, CA, United States Duration: Oct 27 2002 → Oct 31 2002 |
Other
| Other | Air Traffic Management for Commercial and Military Systems |
|---|---|
| Country/Territory | United States |
| City | Irvine, CA |
| Period | 10/27/02 → 10/31/02 |