To read this content please select one of the options below:

Target tracking and enclosing via UAV/UGV cooperation using energy estimation pigeon-inspired optimization and switchable topology

Yankai Shen (Beihang University, Beijing, China)
Chen Wei (Beihang University, Beijing, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 22 December 2022

Issue publication date: 27 March 2023

248

Abstract

Purpose

The research of unmanned air/ground vehicle (UAV/UGV) cooperation has attracted much attention due to its potential applications in disaster rescue and target surveillance. This paper aims to focus on the UAV/UGV cooperative target tracking and enclosing, considering the limits of detection and sensor failures.

Design/methodology/approach

The UAV/UGV cooperation structure is designed, contributing to homogeneous consistency and heterogeneous communication. The target tracking of UAVs is converted into a constraint optimization problem involving tracking cost, and the target enclosing of UGVs is modeled as formation control.

Findings

The energy estimation pigeon-inspired optimization is developed to generate control inputs for UAVs. And the controller combined with switchable topology is proposed, where the switching rule is flexible in dealing with some emergencies.

Practical implications

The proposed structure and algorithms can be easily applied to practice and help design the UAV/UGV control system.

Originality/value

The energy estimation mechanism is proposed for the target tracking of UAVs, and the rules of switching topologies ensure the target enclosing process of UGVs.

Keywords

Acknowledgements

This work was partially supported by the Science and Technology Innovation 2030-Key Project of “New Generation Artificial Intelligence” under grant #2018AAA0102403.

Citation

Shen, Y. and Wei, C. (2023), "Target tracking and enclosing via UAV/UGV cooperation using energy estimation pigeon-inspired optimization and switchable topology", Aircraft Engineering and Aerospace Technology, Vol. 95 No. 5, pp. 768-783. https://doi.org/10.1108/AEAT-05-2022-0143

Publisher

:

Emerald Publishing Limited

Copyright © 2022, Emerald Publishing Limited

Related articles