DocumentCode
3007688
Title
Observability of HEO Satellite Autonomous Navigation System Using GPS
Author
Li, Taohu ; Liu, Jiansheng ; Huang, Zhigang ; Qin, Honglei
Author_Institution
Sch. of Electron. & Inf. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2010
fDate
29-31 Oct. 2010
Firstpage
1
Lastpage
4
Abstract
The high altitudes reached by HEO (highly eccentric orbits) spacecraft present a very unfavorable environment for the reception of GPS signals. This paper analyzed the GPS signal visibility viewed from running HEO spacecraft, and then investigated the observability of the autonomous navigation system with the pseudo-range measurements using a PWCS method , adopted the condition number of the observability matrix as a scalar measure of degree of observability, finally assessed the navigation performance. The results of simulation showed that, with measurements from only one GPS satellite, the observability of the navigation system can be observable; the error of position and velocity could be verified. Therefore, the HEO autonomous navigation using GPS is feasible.
Keywords
Global Positioning System; matrix algebra; space vehicles; GPS satellite; GPS signal reception; HEO satellite autonomous navigation system; HEO spacecraft; PWCS method; observability matrix; Extraterrestrial measurements; Global Positioning System; Observability; Orbits; Satellites; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Multimedia Technology (ICMT), 2010 International Conference on
Conference_Location
Ningbo
Print_ISBN
978-1-4244-7871-2
Type
conf
DOI
10.1109/ICMULT.2010.5631285
Filename
5631285
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