DocumentCode :
2103214
Title :
Design of global positioning system receivers for integrated inertial navigation systems
Author :
Simon, Dan ; El-Sherief, Hossny
Author_Institution :
Systems Integration Group, TRW Inc., Redondo Beach, CA, USA
fYear :
1993
fDate :
15-17 Dec 1993
Firstpage :
1476
Abstract :
There is much interest in integrated navigation using the global positioning system and inertial measurement units (accelerometers and gyroscopes). The results reported in this paper quantify integrated navigation performance as a function of GPS receiver design parameters. The specific application considered is missile navigation
Keywords :
inertial navigation; military systems; missiles; radio receivers; radionavigation; satellite relay systems; accelerometers; design parameters; global positioning system receivers; gyroscopes; inertial measurement units; integrated inertial navigation systems; missile navigation; Accelerometers; Computer errors; Error correction; Filters; Frequency; Global Positioning System; Inertial navigation; Missiles; Phase locked loops; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location :
San Antonio, TX
Print_ISBN :
0-7803-1298-8
Type :
conf
DOI :
10.1109/CDC.1993.325432
Filename :
325432
Link To Document :
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