DocumentCode
1940162
Title
Geometry optimization for GPS navigation
Author
McKay, J.B. ; Pachter, M.
Author_Institution
Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
Volume
5
fYear
1997
fDate
10-12 Dec 1997
Firstpage
4695
Abstract
This paper presents the analysis and numerical optimization of the geometry of an inverted pseudolite positioning system. First, the effect of geometry on the system´s accuracy is examined. The geometric dilution of precision produced by typical system geometry is considered, and an alternate measure of the geometry effect, the condition number of the “visibility” matrix H, is introduced. Next, the optimization of the system´s geometry is presented. The simplified problem of optimizing the geometry with respect to a stationary pseudolite is solved. The results of a numerical optimization are presented and both the effectiveness of the optimization routine and the usefulness of the resulting system configurations are discussed. Finally, design guidelines for good geometry are listed
Keywords
Global Positioning System; aircraft navigation; attitude control; geometry; matrix algebra; optimisation; GPS navigation; aircraft; geometric sensitivity; geometry; global positioning system; inverted pseudolite positioning system; optimization; Accuracy; Aircraft navigation; Computational geometry; Equations; Global Positioning System; Guidelines; Satellite navigation systems; Testing; Transmission line matrix methods; US Government;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
Conference_Location
San Diego, CA
ISSN
0191-2216
Print_ISBN
0-7803-4187-2
Type
conf
DOI
10.1109/CDC.1997.649738
Filename
649738
Link To Document