Robust terrain-aided localization of spacecraft using low-fidelity asteroid shape model

Hirokazu Ishida, Y. Tsuda
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Abstract

We proposed a localization method for spacecraft navigation in the proximity of asteroids. This method uses particle filtering with LIDAR measurement and the terrain data of an asteroid. This type of localization is called terrain-aided localization (TAL), and has been studied intensively in the fields of aeronautics and underwater robotics. However, there exist characteristic difficulties caused by the terrain uncertainty in the application of the TAL to asteroid proximity operations. To overcome these difficulties, we developed a robust terrain-aided localization method, which is effective for general TAL problems unlimited to spacecraft applications. The strength of this method lies in the capability to probabilistically address the collision of a LIDAR ray with an asteroid. The core idea of this method is to perform Monte Carlo sampling at the point at which a LIDAR ray collides with different independently simulated terrains in every trial via stochastic process. This sampling is enabled by utilizing the signed distance function. To confirm the effectiveness of the proposed method, we conducted numerical simulations. The results show the effectiveness of the proposed method.
基于低保真小行星形状模型的航天器鲁棒地形辅助定位
提出了一种用于航天器在小行星附近导航的定位方法。该方法将粒子滤波与激光雷达测量和小行星地形数据结合使用。这种类型的定位被称为地形辅助定位(TAL),在航空和水下机器人领域得到了广泛的研究。然而,地形的不确定性给TAL在小行星接近作战中的应用带来了特征性的困难。为了克服这些困难,我们开发了一种鲁棒地形辅助定位方法,该方法可以有效地解决不受航天器应用限制的一般TAL问题。这种方法的优势在于,它能够从概率上解决激光雷达射线与小行星碰撞的问题。该方法的核心思想是通过随机过程在每次试验中激光雷达射线与不同独立模拟地形碰撞点进行蒙特卡罗采样。这种采样是通过使用带符号距离函数来实现的。为了验证所提方法的有效性,我们进行了数值模拟。实验结果表明了该方法的有效性。
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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