Model-Reference Reinforcement Learning for Safe Aerial Recovery of Unmanned Aerial Vehicles

IF 2.1 3区 工程技术 Q2 ENGINEERING, AEROSPACE
Bocheng Zhao, M. Huo, Ze Yu, Naiming Qi, Jianfeng Wang
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引用次数: 0

Abstract

In this study, we propose an aerial rendezvous method to facilitate the recovery of unmanned aerial vehicles (UAVs) using carrier aircrafts, which is an important capability for the future use of UAVs. The main contribution of this study is the development of a promising method for online generation of feasible rendezvous trajectories for UAVs. First, the wake vortex of a carrier aircraft is analyzed using the finite element method, and a method for establishing a safety constraint model is proposed. Subsequently, a model-reference reinforcementearning algorithm is proposed based on the potential function method, which can ensure the convergence and stability of training. A combined reward function is designed to solve the UAV trajectory generation problem under non-convex constraints. The simulation results show that, compared with the traditional artificial potential field method under different working conditions, the success rate of this method under non-convex constraints is close to 100%, with high accuracy, convergence, and stability, and has greater application potential in the aerial recovery scenario, providing a solution to the trajectory generation problem of UAVs under non-convex constraints.
无人驾驶飞行器安全空中回收的模型参考强化学习
在本研究中,我们提出了一种空中交会方法,以促进使用运载飞机回收无人驾驶飞行器(UAV),这是未来使用无人驾驶飞行器的一项重要能力。本研究的主要贡献在于开发了一种在线生成无人飞行器可行交会轨迹的可行方法。首先,使用有限元法分析了舰载机的尾流涡旋,并提出了建立安全约束模型的方法。随后,提出了一种基于势函数方法的模型参考强化学习算法,该算法可确保训练的收敛性和稳定性。设计了一种组合奖励函数来解决非凸约束条件下的无人机轨迹生成问题。仿真结果表明,与不同工况下的传统人工势场方法相比,该方法在非凸约束条件下的成功率接近100%,具有较高的准确性、收敛性和稳定性,在空中回收场景中具有较大的应用潜力,为非凸约束条件下的无人机轨迹生成问题提供了一种解决方案。
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
Aerospace ENGINEERING, AEROSPACE-
CiteScore
3.40
自引率
23.10%
发文量
661
审稿时长
6 weeks
期刊介绍: Aerospace is a multidisciplinary science inviting submissions on, but not limited to, the following subject areas: aerodynamics computational fluid dynamics fluid-structure interaction flight mechanics plasmas research instrumentation test facilities environment material science structural analysis thermophysics and heat transfer thermal-structure interaction aeroacoustics optics electromagnetism and radar propulsion power generation and conversion fuels and propellants combustion multidisciplinary design optimization software engineering data analysis signal and image processing artificial intelligence aerospace vehicles'' operation, control and maintenance risk and reliability human factors human-automation interaction airline operations and management air traffic management airport design meteorology space exploration multi-physics interaction.
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