Abstract
The design of a flight control for a micro air vehicle type quadrotor is presented. The control scheme is based on a smooth differentiator combined with an adaptive sliding mode controller. The observer provides a smooth and accurate estimation of the full state from partial measurements of state in spite of noise. The adaptive controller guarantee tracking of the desired trajectories against external perturbations. Thus, it can get a smooth measurement helping to adequately calculate the control law and adaptive gains of the controller allows to use a minimal gain sufficiently to keep the sliding mode, but large enough to reject perturbation as they appear. The methodology shows the effectiveness and performance via numerical simulations.
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.
