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Efficient and Optimal Attitude Determination Using Recursive Global Positioning System Signal OperationsIn 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.
Document ID
19980237947
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Crassidis, John L.
(Catholic Univ. of America Washington, DC United States)
Lightsey, E. Glenn
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Markley, F. Landis
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Publication Information
Publication: Journal of Guidance, Control and Dynamics
Subject Category
Aircraft Communications And Navigation
Meeting Information
Meeting: Guidance, Navigation and Control
Location: Boston, MA
Country: United States
Start Date: August 10, 1998
End Date: August 12, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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