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