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Fast integer ambiguity resolution for GPS attitude determination

  • University of Texas at Austin
  • NASA Goddard Space Flight Center

Research output: Contribution to conferencePaperpeer-review

9 Scopus citations

Abstract

In this paper, a new algorithm for GPS 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.

Original languageEnglish
Pages115-123
Number of pages9
DOIs
StatePublished - 1999
EventGuidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States
Duration: Aug 9 1999Aug 11 1999

Conference

ConferenceGuidance, Navigation, and Control Conference and Exhibit, 1999
Country/TerritoryUnited States
CityPortland
Period08/9/9908/11/99

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