Velocity-constrained distributed formation tracking of fixed-wing UAVs with multiple leaders

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
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Abstract

This paper addresses the safety-critical formation tracking of fixed-wing unmanned aerial vehicles, where both the velocity constraint and multiple leaders are taken into consideration. A hierarchical control strategy, consisting of a distributed observer and a formation controller, is elaborately constructed to achieve the desired configuration with the velocity in a safe range. First, a novel distributed observer is designed to estimate the formation error, which promises the practical fixed-time convergence of the estimation error despite unknown inputs of leaders and disturbances. Then, the velocity constraint is enforced through the forward invariance of a safety set, for which a robust control barrier function is carefully constructed considering the effect of disturbances. Further, a local formation controller is established by embedding the robust control barrier function into quadratic programming. Compared with existing results, the proposed controller is able to achieve the formation configuration while satisfying velocity safety, even in the presence of disturbances. Simulations are conducted to demonstrate the proposed method's capability in guaranteeing velocity constraint and stabilizing formation errors.

多领航员固定翼无人机的速度受限分布式编队跟踪
本文探讨了对安全至关重要的固定翼无人飞行器编队跟踪问题,其中同时考虑了速度约束和多领航员问题。本文精心构建了一种由分布式观测器和编队控制器组成的分层控制策略,以实现速度在安全范围内的理想配置。首先,设计了一种新颖的分布式观测器来估计编队误差,尽管有未知的领航员输入和干扰,该观测器仍能保证估计误差的实际固定时间收敛性。然后,通过安全集的前向不变性来强制执行速度约束,并考虑到干扰的影响,精心构建了鲁棒控制障碍函数。此外,通过将鲁棒控制障碍函数嵌入二次编程,建立了局部编队控制器。与现有结果相比,即使存在干扰,所提出的控制器也能在满足速度安全的前提下实现编队配置。仿真证明了所提方法在保证速度约束和稳定编队误差方面的能力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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