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Efficient and optimal attitude determination using recursive global positioning system signal operations

  • NASA Goddard Space Flight Center

Research output: Contribution to conferencePaperpeer-review

5 Scopus citations

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.

Original languageEnglish
Pages1813-1823
Number of pages11
DOIs
StatePublished - 1998
EventGuidance, Navigation, and Control Conference and Exhibit, 1998 - Boston, United States
Duration: Aug 10 1998Aug 12 1998

Conference

ConferenceGuidance, Navigation, and Control Conference and Exhibit, 1998
Country/TerritoryUnited States
CityBoston
Period08/10/9808/12/98

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