Abstract
The article deals with the problem solution of reducing of safety risk level of the navigation and flight control computer system (NAFCCS) of unmanned aerial vehicle (UAV) owing to well-grounded reliability increasing of the NAFCCS critical components. The problem solution lies in development of methods (technique) of calculation of NAFCCS safety risk level, namely probabilities of catastrophic failure occurrence, without Fault Tree Evaluation. The technique allows solving the problems of reducing of safety risk level of the NAFCCS on the systems engineering design stage. The offered technique includes new mathematical models of NAFCCS subsystems with detail presentation of the of critical fault state.
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.
