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System Identification and Control of an Aerobot Drive System

Date

Authors

Pounds, Paul

Mahony, Robert

Corke, Peter Ian

Publisher

Institute of Electrical and Electronics Engineers (IEEE Inc)

Abstract

Fast thrust changes are important for authoritive control of VTOL micro air vehicles. Fixed-pitch rotors that alter thrust by varying rotor speed require high-bandwidth control systems to provide adequate performace. We develop a feedback compensator for

Keywords

Keywords: Aerodynamics; Feedback control; Rotors; Speed; Unmanned aerial vehicles (UAV); VTOL/STOL aircraft; Aerobot drive systems; Feedback compensators; Proportional controllers; Identification (control systems)

URI

http://hdl.handle.net/1885/56483

Collections

ANU Research Publications

Source

Proceedings of 2007 Information, Decision and Control

Type

Conference paper

DOI

10.1109/IDC.2007.374542

Restricted until

2037-12-31

Downloads

File

Description

01_Pounds_System_Identification_and_2007.pdf (1.25 MB)