DocumentCode
2673733
Title
Avionics system for a small unmanned helicopter performing aggressive maneuvers
Author
Gavrilets, V. ; Shterenberg, A. ; Dahleh, M.A. ; Feron, E.
Author_Institution
MIT, Cambridge, MA, USA
Volume
1
fYear
2000
fDate
2000
Abstract
An Xcell.60 5 ft rotor diameter hobby helicopter was instrumented to perform autonomous aggressive maneuvers. Avionics system, state estimator design, and vibration isolation are presented in detail. Analysis of helicopter dynamics based on flight data is given
Keywords
aircraft computers; aircraft control; helicopters; remotely operated vehicles; state estimation; state feedback; transfer functions; vibration isolation; 5 ft; Kalman filter; Xcell.60 hobby helicopter; attitude estimate; autonomous aggressive maneuvers; avionics system; feedback control; helicopter dynamics; high bandwidth servos; small unmanned helicopter; state estimator design; state feedback; transfer functions; vibration isolation; vibration mount design; yaw rate damping; Aerospace electronics; Bandwidth; Batteries; Data acquisition; Feedback control; Helicopters; Robot sensing systems; State estimation; Testing; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location
Philadelphia, PA
Print_ISBN
0-7803-6395-7
Type
conf
DOI
10.1109/DASC.2000.886895
Filename
886895
Link To Document