Abstract
А regressive and an adaptive algorithms of parametric identification of dynamic systems which allow to conduct identification at the nominal modes of operation of the controlled object and satisfy the specified requirements to speed of fading of dynamic processes of identification are offered. The offered algorithms can be applied in the practice of aircraft design for processing the flight information records.
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.
