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