在高空气球上测试神经网络加速器

G. Clark, G. Landis, Ethan Barnes, Blake LaFuente, Kristina Collins
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引用次数: 1

摘要

认知通信项目一直致力于改进人工智能和机器学习方法,以支持它们在空间环境中的部署和持续使用。然而,由于对通用航空电子硬件的计算要求,在空间平台上实施这种技术历来是困难的。虽然存在加速神经网络各方面计算的技术,但此类平台在历史上尚未在太空环境中部署。考虑到在这种环境中测试有效载荷的成本和时间都令人难以承受,高空气球可以作为一种成本低得多的近似空间环境的方法,从而提供了一种成本效益高的方法,用于测试可能更直接部署到航天器上的人工智能硬件加速的新方法。本文描述了一种商用现成的神经网络加速器在高空气球上的成功测试。本文首先解释了我们在评估不同的商用神经网络加速技术时的选择标准:主要考虑因素包括尺寸、重量和功率(SWaP)以及易于集成。其次,介绍了实验飞行测试平台的研制与实现,并对飞行部件和地面部件进行了讨论。然后,本文对实验载荷本身进行了讨论:包括实验步骤以及测试所用的具体图像和方法。最后,论文总结了在高空测试的实验装置以及飞行测试框架本身的评估,确定了如何使用现有平台继续测试商用现货(COTS)加速解决方案。
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Testing a Neural Network Accelerator on a High-Altitude Balloon
The cognitive communications project has been working to refine artificial intelligence and machine learning approaches to support their deployment and sustained use in space environments. It has historically been difficult to implement such techniques on space platforms, however, due to the computational requirements they levy onto general-purpose avionics hardware. While technologies exist to accelerate the computation of aspects of neural networks, such platforms have not historically been deployed in space environments. Given that testing payloads in such environments can be both cost-and time-prohibitive, high-altitude balloons can be used as a way to approximate a space environment at a much lower cost, thus providing a cost-effective way in which to test newer approaches to hardware acceleration for artificial intelligence which may be deployed onto spacecraft more directly. This paper describes a successful test of a commercial off-the-shelf neural network accelerator on a high-altitude balloon. It begins by explaining our selection criteria when evaluating different commercial neural network acceleration techniques: primary considerations include size, weight, and power (SWaP) as well as ease of integration. Next, the paper describes the development and implementation of an experimental flight test platform: flight and ground components are discussed. Afterward, the paper discusses the experimental payload itself: this includes the experimental procedure as well as the specific image and method used for testing. Finally, the paper concludes with an evaluation of both the experimental device tested at altitude as well as the flight test framework itself, identifying how the existing platform can be used to continue testing commercial off-the-shelf (COTS) solutions for acceleration.
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