Design and Testing of an Ultra-Light Weight Perching System for Sloped or Vertical Rough Surfaces on Mars

S. Backus, J. Izraelevitz, Justin Quan, Rianna M. Jitosho, Eitan Slavick, A. Kalantari
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引用次数: 5

Abstract

In this paper, we present the design, characterization, and functional demonstration of a perching system that enables a flying vehicle to land on rough sloped or vertical surfaces. Steep slopes are of particular scientific interest since they are often associated with geologically interesting features including sites of active modification (e.g. landslides/avalanches, slope streaks), exposed bedrock and/or ice, and as-yet unmodified young features (e.g. walls of fresh craters or polar pits that are actively expanding). However the steep nature of these sites makes access with traditional field robots difficult: ground vehicles are unable to traverse the steep terrain and aerial vehicles are limited by their flight time and an ability to operate near terrain. We propose to address these limitation by enabling the UAV to reliably perch on steep terrain to perform in situ measurements and collect samples. Perching also enables a solar powered UAV to traverse large terrain features such as the Valles Marineris that could not be covered in a single flight by repeatedly perching and recharging its batteries. The proposed perching system that is being developed consists of a microspine gripper, a compliant gripper to vehicle interface, and a flying vehicle equipped with an autonomy sensor suite. The system also includes perception and control algorithms that identify perching targets and execute the required perching maneuver. To date, the majority of the effort has focused on developing and characterizing the microspine gripper. The initial prototype weighs 100 g, is capable of securely grasping a range of natural surfaces, and successful grasps support loads of over 10 N. Refinement of the gripper, integrating and testing it on a UAV, measuring aerodynamic disturbances from wall effects, and developing the required perception and control algorithms is ongoing. This paper describes the overall architecture of our proposed system, the design of the gripper, and its performance during initial testing.
火星上倾斜或垂直粗糙表面的超轻型栖息系统的设计与测试
在本文中,我们提出了一种栖息系统的设计、表征和功能演示,该系统使飞行器能够在粗糙的倾斜或垂直表面上着陆。陡坡具有特别的科学意义,因为它们通常与地质上有趣的特征有关,包括活跃的改造场所(例如山体滑坡/雪崩,斜坡条纹),暴露的基岩和/或冰,以及尚未改造的年轻特征(例如新火山口的墙壁或正在积极扩张的极地坑)。然而,这些地点的陡峭性质使得传统的野外机器人难以进入:地面车辆无法穿越陡峭的地形,空中车辆受到飞行时间和近地形操作能力的限制。我们建议通过使无人机能够可靠地停泊在陡峭的地形上进行原位测量和收集样本来解决这些限制。停泊也使太阳能无人机能够穿越像水手谷这样的大型地形特征,这是单次飞行无法通过反复停泊和充电来覆盖的。正在开发的拟议栖息系统包括一个微脊柱夹持器,一个与飞行器接口兼容的夹持器,以及一个配备自主传感器套件的飞行器。该系统还包括识别栖息目标并执行所需栖息机动的感知和控制算法。迄今为止,大部分的努力都集中在开发和表征微脊柱夹持器上。最初的原型机重100克,能够安全地抓取一系列自然表面,并成功抓取超过10牛顿的载荷。对抓取器的改进,在无人机上集成和测试,测量墙壁效应的空气动力学干扰,以及开发所需的感知和控制算法正在进行中。本文描述了我们提出的系统的总体架构,夹具的设计,以及它在初始测试中的性能。
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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