Adaptive Output Feedback for Altitude Control of an Unmanned Helicopter Using Rotor RPM
- 22 June 2004
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Upper bounds for approximation of continuous-time dynamics using delayed outputs and feedforward neural networksIEEE Transactions on Automatic Control, 2003
- Adaptive output feedback control of uncertain nonlinear systems using single-hidden-layer neural networksIEEE Transactions on Neural Networks, 2002
- Adaptive Output Feedback for High-Bandwidth Flight ControlJournal of Guidance, Control, and Dynamics, 2002
- Development of a Reconfigurable Flight Control Law for Tailless AircraftJournal of Guidance, Control, and Dynamics, 2001
- Adaptive Model Inversion Flight Control for Tilt-Rotor AircraftJournal of Guidance, Control, and Dynamics, 1999
- Analysis of Adaptive Neural Networks for Helicopter Flight ControlJournal of Guidance, Control, and Dynamics, 1997
- Multilayer neural-net robot controller with guaranteed tracking performanceIEEE Transactions on Neural Networks, 1996
- Multilayer feedforward networks are universal approximatorsNeural Networks, 1989
- Approximation by superpositions of a sigmoidal functionMathematics of Control, Signals, and Systems, 1989
- On the approximate realization of continuous mappings by neural networksNeural Networks, 1989