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NASA NTRS · 19990063852

Fast Integer Ambiguity Resolution for GPS Attitude Determination

Abstract

In this paper, a new algorithm for GPS (Global Positioning System) integer ambiguity resolution is shown. The algorithm first incorporates an instantaneous (static) integer search to significantly reduce the search space using a geometric inequality. Then a batch-type loss function is used to check the remaining integers in order to determine the optimal integer. This batch function represents the GPS sightline vectors in the body frame as the sum of two vectors, one depending on the phase measurements and the other on the unknown integers. The new algorithm has several advantages: it does not require an a-priori estimate of the vehicle's attitude; it provides an inherent integrity check using a covariance-type expression; and it can resolve the integers even when coplanar baselines exist. The performance of the new algorithm is tested on a dynamic hardware simulator.

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BibTeXRIS

Lightsey, E. Glenn, Crassidis, John L., Markley, F. Landis. 1999-01-01. Fast Integer Ambiguity Resolution for GPS Attitude Determination. https://ntrs.nasa.gov/citations/19990063852

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