Abstract
Abstract In this paper, stage optimization is addressed with midcourse guidance laws. In case of the optimal control, it is the optimal solution for a single scenario. Therefore, in order to apply the optimal control input to various scenarios, it should be stored, interpolated and used in an open loop form. In this paper, the real-time guidance laws used in anti-air missiles are considered. The parameters included in the guidance commands and stage weights are defined as optimization objective parameters. The result of weight optimization using guidance laws and optimal control input were compared, the difference in stage weights results occurs from 4 kg to 16 kg.
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.
