Abstract
The development of unmanned aircraft requires the development of automatic control systems for unmanned aerial vehicles. The main purpose of such control is to ensure the landing of a unmanned aerial vehicle. Landing can be considered as problem of ensuring a given glide path, which must be observed in case of vary in mass and changing unmanned aerial vehicles dynamic properties near the surface of the earth. The aim of this article is to provide analysis of perspectives in applying variable structure systems for unmanned aerial vehicles landing control with implemented sliding (quasi-sliding) motion mode where glide path is set by a function of system structure switching.
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.
