DocumentCode
1130376
Title
Range Correlation Guidance for Cruise Missiles
Author
Reed, C.G. ; Hocan, J.J.
Author_Institution
Goodyear Aerospace Corporation
Issue
4
fYear
1979
fDate
7/1/1979 12:00:00 AM
Firstpage
547
Lastpage
554
Abstract
A dual-mode position updating system for extended long-range cruise missiles is presented. During either extremely high-or low-altitude cruise missile flight, this system can periodically establish the actual position of the cruise missile by comparing prestored reference data with radar-return data obtained from an onboard conventional radar operated in either a range-only or an altimeter mode. The general features of this position updating system and details of the range-only concept are presented. This includes a discription of the radar system, the data processor, the prestored reference data, and the system performance characteristics.
Keywords
Costs; Cultural differences; Kalman filters; Land vehicles; Missiles; Radar; Remotely operated vehicles; Road vehicles; System performance; Weapons;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1979.308739
Filename
4102192
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