Abstract
We consider a three-body conflict problem in which an aerial target is pursued by a homing missile, and the target launches a defense missile to intercept the homing missile. Under the assumption that the homing missile adopts a proportional guidance law with more maneuverability than aerial target and defense missile, we propose a cooperative robust line of sight guidance law based on a nonlinear control method. Simulations are carried out for the different levels of cooperation and compared with the traditional proportional guidance law, showing the better performance of proposed guidance law.
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.
