DocumentCode :
3032618
Title :
Preliminary orbit design of hybrid navigation constellation
Author :
Lei, Han ; Cong-ying, Li ; Xiao, Yang
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
222
Lastpage :
227
Abstract :
On the basis of the Compass geostationary navigation satellite program, the paper gives the preliminary orbit design of hybrid navigation constellation considering the satellite visibility and geometric dilution of precision (GDOP). The simulation results show that positioning accuracy of the hybrid constellation is significantly higher than GPS and Galileo, especially for China, its surroundings and high latitudes areas considering the same measuring precision of the pseudorange. The orbit design can meet the need of global and regional navigation.
Keywords :
satellite navigation; Compass geostationary navigation satellite program; GPS; Galileo; geometric dilution of precision; global navigation; hybrid navigation constellation; positioning accuracy; preliminary orbit design; regional navigation; satellite visibility; Global Positioning System; GDOP; Hybrid Constellation; Orbit Design; Satellite visibility;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5632561
Filename :
5632561
Link To Document :
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