System Identification and Control of an Aerobot Drive System
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
|Collections||ANU Research Publications|
|Source:||Proceedings of 2007 Information, Decision and Control|
|01_Pounds_System_Identification_and_2007.pdf||1.28 MB||Adobe PDF||Request a copy|
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