DocumentCode :
1255721
Title :
Attitude determination with GPS: experimental results
Author :
Martin-Neira, M. ; Lucas, R. ; Martínez, M.A.
Author_Institution :
ESA, ESTEC, Noordwijk, Netherlands
Volume :
5
Issue :
9
fYear :
1990
Firstpage :
24
Lastpage :
29
Abstract :
An approach to global positioning system (GPS) attitude determination and the results of an experimental evaluation are presented. The most outstanding features of the method are the fundamental observable used for attitude calculation, the triple difference, and the introduction of a new parameter, the differential dilution of precision (DDOP), which relates the GPS satellite geometry to the GPS accuracy when measuring angular magnitudes. The experiment used two commercial off-the-shelf GPS C/A code receivers delivering integrated Doppler measurements. The algorithm is robust with respect to phase cycle slips and does not require solving the usual integer ambiguity of the measurements. The preliminary results show that absolute attitude determination requires a calibration of the baseline and that the relative attitude accuracy is on the order of 0.1 degrees or 2 mrads for the case of a 2-m-long baseline.<>
Keywords :
attitude control; radionavigation; satellite relay systems; spatial variables measurement; GPS; angular magnitudes; baseline; calibration; global positioning system; integrated Doppler measurements; phase cycle slips; radionavigation; satellite geometry; Aircraft navigation; Doppler measurements; Extraterrestrial measurements; Geometry; Global Positioning System; Phase measurement; Position measurement; Robustness; Satellites; Space vehicles;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/62.59282
Filename :
59282
Link To Document :
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