Abstract
AbstractHybrid aircrafts are unique type of aircrafts that combine the hover capability of helicopters with the speed and range of airplanes. In this work, we propose a novel hybrid aircraft based on the fixed-wing airplane and quadrotor structures. A complete mathematical model of the aircraft, in helicopter, transition and airplane flight modes is presented. Furthermore, a nonlinear controller for stabilizing the aircraft at hover is proposed. Finally, simulation results are presented in order to illustrate performances of the proposed controller.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
