Abstract
Sequential quadratic programming is used to solve a minimum-noise aircraft landing-approach problem for two dynamic models. The “exact” model features the usual point-mass equations of motion for flight in a vertical plane. The other model is based on two simplifying assumptions: (1) small angle of attack and flight path angle and (2) no flight path angle dynamics (lift equals weight). Range is used to replace time as the independent variable. The resulting models are of order three and two, respectively; each model involves two control functions. The primary objective is to compare the solutions for each model with regard to accuracy and computational effort. Numerical results are presented for a variety of boundary conditions and path constraints.
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 callMore From: Control Applications of Nonlinear Programming and Optimization
Disclaimer: 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.
