On-board modeling of gravity fields of elongated asteroids using Hopfield neural networks

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Astrodynamics Pub Date : 2022-11-05 DOI:10.1007/s42064-022-0151-3
Yingjie Zhao, Hongwei Yang, Shuang Li, Yirong Zhou
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引用次数: 1

Abstract

To rapidly model the gravity field near elongated asteroids, an intelligent inversion method using Hopfield neural networks (HNNs) is proposed to estimate on-orbit simplified model parameters. First, based on a rotating mass dipole model, the gravitational field of asteroids is characterized using a few parameters. To solve all the parameters of this simplified model, a stepped parameter estimation model is constructed based on different gravity field models. Second, to overcome linearization difficulties caused by the coupling of the parameters to be estimated and the system state, a dynamic parameter linearization technique is proposed such that all terms except the parameter terms are known or available. Moreover, the Lyapunov function of the HNNs is matched to the problem of minimizing parameter estimation errors. Equilibrium values of the Lyapunov function are used as estimated values. The proposed method is applied to natural elongated asteroids 216 Kleopatra, 951 Gaspra, and 433 Eros. Simulation results indicate that this method can estimate the simplified model parameters rapidly, and that the estimated simplified model provides a good approximation of the gravity field of elongated asteroids.

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利用Hopfield神经网络对细长小行星的重力场进行星载建模
为了快速建立细长小行星附近的重力场模型,提出了一种基于Hopfield神经网络(HNNs)的在轨简化模型参数估计智能反演方法。首先,基于旋转质量偶极子模型,利用几个参数对小行星引力场进行表征。为了求解该简化模型的所有参数,建立了基于不同重力场模型的阶梯式参数估计模型。其次,为了克服因待估计参数与系统状态耦合而造成的线性化困难,提出了一种除参数项外的所有项都已知或可用的动态参数线性化技术。此外,hnn的Lyapunov函数与参数估计误差最小化问题相匹配。用李雅普诺夫函数的平衡值作为估计值。所提出的方法适用于自然细长的小行星216 Kleopatra, 951 Gaspra和433 Eros。仿真结果表明,该方法能快速估计出简化模型参数,简化模型能较好地逼近细长小行星的重力场。
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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