Surfing vortex rings for energy-efficient propulsion.

IF 2.2 Q2 MULTIDISCIPLINARY SCIENCES
PNAS nexus Pub Date : 2025-02-25 eCollection Date: 2025-02-01 DOI:10.1093/pnasnexus/pgaf031
Peter Gunnarson, John O Dabiri
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引用次数: 0

Abstract

Leveraging background fluid flows for propulsion has the potential to enhance the range and speed of autonomous aerial and underwater vehicles. In this work, we demonstrate experimentally a fully autonomous strategy for exploiting vortex rings for energy-efficient propulsion. First, an underwater robot used an onboard inertial measurement unit (IMU) to sense the motion induced by the passage of a vortex ring generated by a thruster in a 13,000-L water tank. In response to the sensed acceleration, an impulsive maneuver entrained the robot into the material boundary of the vortex ring. After entrainment, the robot was propelled across the tank without expending additional energy or control effort. By advecting with the vortex ring, the robot achieved a nearly fivefold reduction in the energy required to traverse the tank compared to swimming in quiescent flow. Using the controlled finite-time Lyapunov exponent field and corresponding Lagrangian coherent structures, we analyze and explain the initial entrainment process and the sensitivity to the starting time and position of the surfing maneuver. Additionally, linear acceleration as sensed by the onboard IMU was found to correspond with the pressure gradient of the background flow, and rotational acceleration is suggested as a method for measuring the vorticity of the vortex ring. This study serves as a proof-of-concept demonstration of the potential for onboard inertial measurements to enable efficient interaction with background fluid flows.

利用背景流体流进行推进,有可能提高自主飞行器和水下航行器的航程和速度。在这项工作中,我们通过实验展示了一种利用涡环进行节能推进的全自主策略。首先,一个水下机器人使用一个机载惯性测量单元(IMU)来感知推进器在一个 13000 升的水箱中产生的涡环通过时引起的运动。针对感应到的加速度,一个脉冲机动装置将机器人卷入涡流环的材料边界。夹带后,机器人被推过水箱,无需消耗额外的能量或控制力。与在静止流中游动相比,通过与涡流环贴合,机器人穿越水箱所需的能量减少了近五倍。利用受控的有限时间 Lyapunov 指数场和相应的拉格朗日相干结构,我们分析并解释了初始夹带过程以及对冲浪动作的开始时间和位置的敏感性。此外,我们还发现机载 IMU 感知到的线性加速度与背景流的压力梯度相对应,并建议将旋转加速度作为测量涡环涡度的一种方法。这项研究作为概念验证,展示了机载惯性测量与背景流体流有效互动的潜力。
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
CiteScore
1.80
自引率
0.00%
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