DocumentCode :
35078
Title :
Low-Complexity Instantaneous Ambiguity Resolution with the Affine-Constrained GNSS Attitude Model
Author :
Giorgi, Giada ; Teunissen, Peter J. G.
Author_Institution :
Inst. for Commun. & Navig., Munich Univ. of Technol., Munich, Germany
Volume :
49
Issue :
3
fYear :
2013
fDate :
Jul-13
Firstpage :
1745
Lastpage :
1759
Abstract :
In this contribution a new approach to ambiguity resolution for Global Navigation Satellite System (GNSS)-based attitude estimation applications is discussed and tested. This approach enhances the observation model by means of additional linear constraints. These constraints are implicitly derived by applying an affine transformation to the unknown real-valued parameters, and largely aid the integer ambiguity estimation through an improved float estimation. The new method is characterized by a lower computational complexity than a rigorous nonlinearly-constrained GNSS attitude model, and at the same time it guarantees higher performance than unconstrained, and therefore weaker, models. The ambiguity resolution performance of the affine-constrained approach is tested through a series of simulated as well as actual data sets, demonstrating the validity and usefulness of the proposed approach for multi-antenna GNSS-based attitude determination applications.
Keywords :
aerospace instrumentation; attitude measurement; satellite navigation; affine constrained GNSS attitude model; affine transformation; attitude estimation; float estimation; global navigation satellite system; integer ambiguity estimation; linear constraints; low complexity instantaneous ambiguity resolution; multiantenna GNSS based attitude determination; unknown real valued parameter; Antennas; Computational modeling; Educational institutions; Estimation; Global Navigation Satellite Systems; Minimization; Position measurement;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2013.6558017
Filename :
6558017
Link To Document :
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