Abstract
AbstractThe nonlinear flight dynamics of a rigid body aircraft is stabilized using a modified output feedback linearization control. The perturbations and model uncertainties effects are canceled out by the injection of a compensation term computed by the application of High-Order Sliding Mode Observers-Identifiers. The feedback linearizing controller is designed considering a nominal model of the aircraft dynamic. The resulting controller exhibits a high robustness guaranteeing the stability and maneuverability of the aircraft in the presence of system uncertainties and external perturbations.
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.
