DocumentCode
2897816
Title
Navigational needs for current and future high-G inertial measurement units
Author
Killen, Albert K.
Author_Institution
US Army Missile Command, Redstone Arsenal, AL, USA
fYear
1992
fDate
23-27 Mar 1992
Firstpage
141
Lastpage
146
Abstract
The author uses the ADKEM (advanced kinetic energy missile) IMU (inertial measurement unit) performance requirements as a platform to discuss various error sources and their contribution to the ADKEM system performance and to indicate possible applications of this technology for the future. Particular attention is given to the ADKEM IMU error budget
Keywords
aerospace instrumentation; inertial navigation; measurement errors; missiles; advanced kinetic energy missile; error budget; error sources; future; high-G inertial measurement units; inertial navigation; performance requirements; Acceleration; Aircraft; Costs; Helicopters; Hidden Markov models; Instruments; Kinetic energy; Measurement units; Missiles; Navigation;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 1992. Record. 500 Years After Columbus - Navigation Challenges of Tomorrow. IEEE PLANS '92., IEEE
Conference_Location
Monterey, CA
Print_ISBN
0-7803-0468-3
Type
conf
DOI
10.1109/PLANS.1992.185832
Filename
185832
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