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NASA NTRS · 19980237947

Efficient and Optimal Attitude Determination Using Recursive Global Positioning System Signal Operations

Abstract

In this paper, a new and efficient algorithm is developed for attitude determination from Global Positioning System signals. The new algorithm is derived from a generalized nonlinear predictive filter for nonlinear systems. This uses a one time-step ahead approach to propagate a simple kinematics model for attitude determination. The advantages of the new algorithm over previously developed methods include: it provides optimal attitudes even for coplanar baseline configurations; it guarantees convergence even for poor initial conditions; it is a non-iterative algorithm; and it is computationally efficient. These advantages clearly make the new algorithm well suited to on-board applications. The performance of the new algorithm is tested on a dynamic hardware simulator. Results indicate that the new algorithm accurately estimates the attitude of a moving vehicle, and provides robust attitude estimates even when other methods, such as a linearized least-squares approach, fail due to poor initial starting conditions.

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BibTeXRIS

Crassidis, John L., Lightsey, E. Glenn, Markley, F. Landis. 1998-01-01. Efficient and Optimal Attitude Determination Using Recursive Global Positioning System Signal Operations. https://ntrs.nasa.gov/citations/19980237947

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