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Vision-based Guidance for Loitering over a Target

  • Received : 2016.01.05
  • Accepted : 2016.09.21
  • Published : 2016.09.30

Abstract

This paper presents a vision-based guidance method that allows a fixed-wing aircraft to orbit around a target at a given radius. The guidance method uses a simple formula that regulates a relative side-bearing angle estimated by a vision system. The global asymptotic stability of the associated guidance law is demonstrated, and a linear analysis is performed to facilitate the proper selection of the relevant control parameters. A flight experiment is presented to demonstrate the feasibility and performance of the proposed guidance method.

Keywords

References

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  2. Vision-Based Tracking of a Ground-Moving Target with UAV pp.2093-2480, 2019, https://doi.org/10.1007/s42405-019-00142-z