Abstract

An evasion guidance method based on virtual goals is proposed for re-entry vehicles to avoid a no-fly zone. The guidance method combined with the Dubins curve path planning method and proportion guidance can effectively avoid the no-fly zone based on the maneuverability analysis of the re-entry vehicle. This method designed an energy-based motion model combined with the Quasi equilibrium glide conditions, enabling the prediction-correction guidance to correct the errors caused by evasion and meet the altitude as well as voyage constraints. The simulation shows that the evasion guidance method can effectively avoid the no-fly zone, meet the re-entry terminal constraints, and the algorithm is robust and adaptable.

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 call

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.