Nonlinear adaptive model following control for a 3-DOF tandem-rotor model helicopter
Authors:
- Mitsuaki IshitobiMIMitsuaki Ishitobi
- Masatoshi NishiMNMasatoshi Nishi
- Kazuhide NakasakiKNKazuhide Nakasaki
- 1 August 2010
- journal article
- Published by Elsevier in Control Engineering Practice
- Vol. 18 (8) , 936-943
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Robust design of a spacecraft attitude tracking control system with actuator uncertainties2008
- Robust full degree-of-freedom tracking control of a helicopterAutomatica, 2007
- Design and flight testing of various H∞ controllers for the Bell 205 helicopterControl Engineering Practice, 2005
- Experimental results on adaptive output feedback control using a laboratory model helicopterIEEE Transactions on Control Systems Technology, 2005
- Robust trajectory tracking for a scale model autonomous helicopterInternational Journal of Robust and Nonlinear Control, 2004
- A flight control system for aerial robots: algorithms and experimentsControl Engineering Practice, 2003
- NONLINEAR CONTROL FOR A TANDEM ROTOR HELICOPTERIFAC Proceedings Volumes, 2002
- Mixed Norm Control of a HelicopterJournal of Guidance, Control, and Dynamics, 2001
- Output tracking control design of a helicopter model based on approximate linearization1998
- Dynamical sliding mode control approach for vertical flight regulation in helicoptersIEE Proceedings - Control Theory and Applications, 1994