Flight Testing of a Gain-Scheduled Stability and Control Augmentation System for a Quad-Tilt-Wing UAV
AIAA Guidance, Navigation, and Control Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2016
|British Library Conference Proceedings | 2015
|Design of flight control system for quad tilt-wing UAV
IEEE | 2015
|Towards gain-scheduled Hinfinity control design for a tilt-wing aircraft
Tema Archiv | 2004
|