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Optimal integer resolution for attitude determination using global positioning system signalsIn this paper, a new motion-based algorithm for GPS integer ambiguity resolution is derived. The first step of this algorithm converts the reference sightline vectors into body frame vectors. This is accomplished by an optimal vectorized transformation of the phase difference measurements. The result of this transformation leads to the conversion of the integer ambiguities to vectorized biases. This essentially converts the problem to the familiar magnetometer-bias determination problem, for which an optimal and efficient solution exists. Also, the formulation in this paper is re-derived to provide a sequential estimate, so that a suitable stopping condition can be found during the vehicle motion. The advantages of the new algorithm include: 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 sequentially estimate the ambiguities during the vehicle motion. The only disadvantage of the new algorithm is that it requires at least three non-coplanar baselines. The performance of the new algorithm is tested on a dynamic hardware simulator.
Document ID
19980203805
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Crassidis, John L.
(Catholic Univ. of America Washington, DC United States)
Markley, F. Landis
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Lightsey, E. Glenn
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
August 18, 2013
Publication Date
May 1, 1998
Publication Information
Publication: AAS/GSFC 13th International Symposium on Space Flight Dynamics
Volume: 1
Subject Category
Astrodynamics
Report/Patent Number
AAS-98-331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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