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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 journalArticlepeer-review

41 Scopus citations

Abstract

A new and efficient algorithm is developed for attitude determination from global positioning system signals. The new algorithm is derived from a generalized 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 noniterative algorithm, and it is computationally efficient. These advantages clearly make the new algorithm well suited to onboard 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
Pages (from-to)193-201
Number of pages9
JournalJournal of Guidance, Control, and Dynamics
Volume22
Issue number2
DOIs
StatePublished - 1999

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