一种用于航天器姿态和轨道确定的高斯确定性平滑和预测方法

Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093) Pub Date : 2000-10-10 DOI:10.1109/NAECON.2000.894980

M.S. Hodgart, P. Tortora, N. Morrison

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引用次数: 4

摘要

给出了一些理论，并结合仿真结果，确定了一种卡尔曼滤波器风格的滤波器/估计器。相对于典型卫星(和其他)应用中常用的滤波器，它有一些显著的优势。我们称其为衰落高斯确定性滤波器，并概述了其主要特征。

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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A Gaussian deterministic approach to smoothing and prediction for application to spacecraft attitude and orbit determination

Some theory is presented, with results from simulation, that identify a filter/estimator in the style of the Kalman filter. It promises some significant advantages relative to the usual filter in typical satellite (and other) applications. We call it a fading Gaussian deterministic filter and outline its main features.

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来源期刊

Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093)

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