Abstract
Digital fly-by-wire flight control systems are currently of interest because simple mechanical linkages are no longer able to cope with the many control problems associated with high performance aircraft. In view of this, a digital adaptive flight control algorithm has been developed by combining a weighted least squares estimator with optimal linear regulator control logic designed to minimize a quadratic model following performance index. Results for a typical fighter aircraft's trajectory over six distinct flight conditions are very promising.
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.
