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

Aerospace Engineering and Mechanics

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

20 Scopus citations

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

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@inproceedings{252576464e0342a19810b9ca561d9eca,

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",

year = "2002",

month = jan,

day = "1",

language = "English (US)",

volume = "2",

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

note = "Air Traffic Management for Commercial and Military Systems ; Conference date: 27-10-2002 Through 31-10-2002",

}

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.

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 - https://www.scopus.com/pages/publications/0036451929

UR - https://www.scopus.com/pages/publications/0036451929#tab=citedBy

M3 - Conference contribution

AN - SCOPUS:0036451929

VL - 2

BT - AIAA/IEEE Digital Avionics Systems Conference - Proceedings

T2 - Air Traffic Management for Commercial and Military Systems

Y2 - 27 October 2002 through 31 October 2002

ER -

Flight test and simulation results for an autonomous aerobatic helicopter

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