DocumentCode :
860482
Title :
Integrated strapdown avionics for precision guided weapons
Author :
Richman, Jack ; Haessig, David, Jr. ; Friedland, Bernard
Author_Institution :
Singer Company, Little Falls, NJ, USA
Volume :
6
Issue :
3
fYear :
1986
fDate :
6/1/1986 12:00:00 AM
Firstpage :
9
Lastpage :
12
Abstract :
Conventional avionic configurations for precision guided weapons are often unnecessarily costly and inefficient because of built-in (but unused) redundancy in instrumentation attributed to the present day independent systems design approach. Described in this paper is an integrated design approach using strapdown avionic components that has the potential for lowering cost, increasing reliability, and improving overall performance as a result of using fewer and less costly instruments in an efficient manner.
Keywords :
Inertial navigation; Missile guidance; Acceleration; Accelerometers; Aerospace electronics; Automotive engineering; Costs; Instruments; Lifting equipment; Navigation; Redundancy; Weapons;
fLanguage :
English
Journal_Title :
Control Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0272-1708
Type :
jour
DOI :
10.1109/MCS.1986.1105094
Filename :
1105094
Link To Document :
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