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

M.S. Hodgart, P. Tortora, N. Morrison
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引用次数: 4

Abstract

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.
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
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。
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