Coordinated Formation Guidance Law for Fixed-Wing UAVs Based on Missile Parallel Approach Method

Coordinated Formation Guidance Law for Fixed-Wing UAVs Based on Missile Parallel Approach Method

This paper presents a classic missile-type parallel-approach guidance law for fixed-wing UAVs in coordinated formation flight. The key idea of the proposed guidance law is to drive each follower to follow the virtual target point. Considering the turning ability of each follower, the formation form...

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Bibliographic Details
Main Authors: Zheng Gong, Zan Zhou, Zian Wang, Quanhui Lv, Jinfa Xu, Yunpeng Jiang
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Aerospace
Subjects:
fixed-wing UAVs
formation flight
guidance law
semi-perfect rigid formation
flight test
Online Access:https://www.mdpi.com/2226-4310/9/5/272

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