Flight test and simulation results for an autonomous aerobatic helicopter

V. Gavrilets; I. Martinos; B. Mettler; E. Feron

Flight test and simulation results for an autonomous aerobatic helicopter

V. Gavrilets, I. Martinos, B. Mettler, E. Feron

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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
State	Published - Jan 1 2002
Externally published	Yes

Cite this

@inproceedings{6cd7b2c431404650b5a17efa683a4999,

title = "Flight test and simulation results for an autonomous aerobatic helicopter",

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.",

author = "V. Gavrilets and I. Martinos and B. Mettler and E. Feron",

note = "Generated from Scopus record by KAUST IRTS on 2021-02-18",

year = "2002",

month = jan,

day = "1",

language = "English (US)",

booktitle = "AIAA/IEEE Digital Avionics Systems Conference - Proceedings",

}

TY - GEN

T1 - Flight test and simulation results for an autonomous aerobatic helicopter

AU - Gavrilets, V.

AU - Martinos, I.

AU - Mettler, B.

AU - Feron, E.

N1 - Generated from Scopus record by KAUST IRTS on 2021-02-18

PY - 2002/1/1

Y1 - 2002/1/1

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=0036451929&partnerID=8YFLogxK

M3 - Conference contribution

BT - AIAA/IEEE Digital Avionics Systems Conference - Proceedings

ER -

Flight test and simulation results for an autonomous aerobatic helicopter

Abstract

Other files and links

Fingerprint

Cite this