Analysis of rendezvous guidance laws for autonomous aerial refueling for non-maneuvering and identical speed targets

نویسندگان

چکیده

This study analyzes rendezvous guidance schemes for UAVs refueling. Assuming the target is non-maneuvering with identical speed, a necessary condition investigated UAV to approach point. Three types of laws are considered analyze performance under condition. A reachable region analytically obtained using closed-form solution deviated pursuit and pure proportional navigation. Numerical simulation demonstrates analyzed result mission.

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ژورنال

عنوان ژورنال: Aerospace Science and Technology

سال: 2022

ISSN: ['1626-3219', '1270-9638']

DOI: https://doi.org/10.1016/j.ast.2022.107359