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NASA NTRS · 19970017209

A Predictive Attitude Determination Algorithm

Abstract

In this paper, a new and efficient algorithm is developed for attitude determination from vector observations. The new algorithm, called the Predictive Attitude Determination (PAD) algorithm, is derived from a general nonlinear predictive filter approach. Traditional deterministic algorithms are shown to be suboptimal for anisotropic measurement errors. The major advantage of the PAD algorithm is that it can be easily applied to the case where anisotropic measurement errors exist. Also, an analytical expression is derived for the steady-state attitude error covariance, which is shown to be equivalent to the optimal covariance derived from maximum likelihood techniques. Simulation studies indicate that the new algorithm is able to accurately determine the attitude of a spacecraft, even for radically anisotropic measurement errors.

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BibTeXRIS

Markley, F. Landis, Crassidis, John L.. 1997-05-01. A Predictive Attitude Determination Algorithm. https://ntrs.nasa.gov/citations/19970017209

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