Abstract
This paper concentrates on attitude control and tracking control about the hex-rotor Unmanned Aerial Vehicle (UAV). This kind of aircraft is a nonlinear, coupled MIMO system. Considering the model uncertainties and the external disturbances, good robustness is one of the key factors for the UAV. Based on the characteristics of the hex-rotor UAV model, nonlinear H\( \infty \) controller and adaptive backstepping sliding mode controller are designed to realize the attitude and position control respectively. And the control strategies are verified by the simulation. It’s proved that the control system has strong robustness to both the disturbance and the parametric variation.
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.
