DocumentCode
1722340
Title
Simulation Research on Feasibility of the Shipborne Pseudolite for GPS Augmentation
Author
Gannan, Yuan ; Xingli, Gan ; Kewen, Wang
Author_Institution
Harbin Engineering University, Harbin 150001 China
fYear
2007
Abstract
In allusion to the need of high-precision and high-stability navigation system in the airplane during taking off and landing process, a original shipborne pseudolite for augmenting GPS has been put forward. The feasibility of shipborne mobile pseudolite has been analyzed by comparing with the airborne pseudolite, and the performance of shipborne pseudolite is superiority over one of airborne pseudolite´s. Geometric Dilution of precision (GDOP) is deduced from the pseudo-distance error, it is approved that GDOP can be reduced by using shipborne pseudolite and the difficulty of GPS receiver select satellites is debased, the select satellites method which calculated the maximum volume of four GPS projected tetrahedron is simplified to calculated the maximum area of three GPS projected triangle. By the way of simulation, the variable trend is analyzed quantificationally between GPS augmentation back and forth, while GPS vertical angle varies from 0deg to 70deg and pseudolite vertical angle varies from -15deg to -90deg, the navigation system has a optimum performance.
Keywords
Global Positioning System; aircraft navigation; radio receivers; GPS augmentation; GPS receiver; Global Positioning System; airplane; geometric dilution of precision; high-precision navigation system; high-stability navigation system; pseudodistance error; select satellites method; shipborne mobile pseudolite; shipborne pseudolite; Aircraft navigation; Airplanes; Analytical models; Frequency; Gallium nitride; Global Positioning System; Instruments; Performance analysis; Position measurement; Satellites; GDOP; GPS; Shipborne Pseudolite; VDOP;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronic Measurement and Instruments, 2007. ICEMI '07. 8th International Conference on
Conference_Location
Xi´an
Print_ISBN
978-1-4244-1136-8
Electronic_ISBN
978-1-4244-1136-8
Type
conf
DOI
10.1109/ICEMI.2007.4350634
Filename
4350634
Link To Document