10.1109/CHICC.2006.2809222006 Chinese Control Conference Proceedings, CCC 20062087-209
Designing high performance control of rotorcraft unmanned aerial vehicle (UAV) requires a mathematic...
For realizing the yaw-heave coupling control of unmanned helicopters in full flight envelope, an act...
With the characteristics of input nonlinearity, time-varying parameters and the couplings between ma...
10.1109/TIE.2008.926780IEEE Transactions on Industrial Electronics5593426-3434ITIE
10.1109/CDC.2007.4434213Proceedings of the IEEE Conference on Decision and Control1963-1968PCDC
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the ...
10.1109/MED.2006.32886014th Mediterranean Conference on Control and Automation, MED'06
This paper explains the methodology developed to design the yaw control system (heading control syst...
Includes bibliographical references (leaf 55)The purpose of this project is to find a parsimonious m...
10.1109/CHICC.2006.4347398Proceedings of the 26th Chinese Control Conference, CCC 2007662-66
Dissertation (Ph.D.)--University of Kansas, Aerospace Engineering, 2007.There has been a significant...
We consider the problem of controlling the vertical, lateral and longitudinal motion of a nonlinear ...
Abstract- Unmanned Aerial Vehicle become popular and very useful today. Unmanned Aerial Vehicle type...
Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helic...
This paper studies the multi-source disturbances attenuation problem on the yaw motion of unmanned a...
Designing high performance control of rotorcraft unmanned aerial vehicle (UAV) requires a mathematic...
For realizing the yaw-heave coupling control of unmanned helicopters in full flight envelope, an act...
With the characteristics of input nonlinearity, time-varying parameters and the couplings between ma...
10.1109/TIE.2008.926780IEEE Transactions on Industrial Electronics5593426-3434ITIE
10.1109/CDC.2007.4434213Proceedings of the IEEE Conference on Decision and Control1963-1968PCDC
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the ...
10.1109/MED.2006.32886014th Mediterranean Conference on Control and Automation, MED'06
This paper explains the methodology developed to design the yaw control system (heading control syst...
Includes bibliographical references (leaf 55)The purpose of this project is to find a parsimonious m...
10.1109/CHICC.2006.4347398Proceedings of the 26th Chinese Control Conference, CCC 2007662-66
Dissertation (Ph.D.)--University of Kansas, Aerospace Engineering, 2007.There has been a significant...
We consider the problem of controlling the vertical, lateral and longitudinal motion of a nonlinear ...
Abstract- Unmanned Aerial Vehicle become popular and very useful today. Unmanned Aerial Vehicle type...
Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helic...
This paper studies the multi-source disturbances attenuation problem on the yaw motion of unmanned a...
Designing high performance control of rotorcraft unmanned aerial vehicle (UAV) requires a mathematic...
For realizing the yaw-heave coupling control of unmanned helicopters in full flight envelope, an act...
With the characteristics of input nonlinearity, time-varying parameters and the couplings between ma...
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