Abstract
SummaryA mathematical model is presented of the aircraft program flight along a predetermined trajectory, with or without a specified speed history. Moreover, the aircraft is constrained to coordinated turns, which implies zero value of sideslip angle. The final equations of program motion are derived as a set of differential/algebraic equations. The aircraft control input ensuring the exact realisation of program constraints results from the transient dynamic solution of the equations of program motion. A simple numerical illustration is included.
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.
