DocumentCode
3386720
Title
Ring laser gyro applications for tactical missiles: the Army TACMS solution
Author
Curran, George L. ; Engelken, Daniel J.
Author_Institution
Honeywell Mil. Avionics Div., Clearwater, FL, USA
fYear
1990
fDate
20-23 Mar 1990
Firstpage
543
Lastpage
548
Abstract
The Honeywell H700-3A ring laser gyro missile guidance set (AN/DJW-51) provides navigation, guidance, autopilot, weapons dispensing, and communications functions for the US Army TACMS missile in a low-initial-cost and low-life-cycle-cost package. It is primarily the use of low-cost inertial sensors which make the use of a ring laser gyro navigation system feasible in the tactical missile market. The H700-3A ring laser gyro missile guidance set has proven to be a low-cost, high-accuracy guidance and navigation system for the deep-strike Army missile weapons system. This has been borne out by a highly successful test program of 26 missile flights. The components of the missile guidance set are described in detail
Keywords
aerospace computer control; gyroscopes; inertial navigation; laser beam applications; missiles; ring lasers; AN/DJW-51; Army TACMS solution; Honeywell H700-3A ring laser gyro missile guidance set; autopilot; communications functions; guidance; navigation; tactical missiles; weapons dispensing; Accelerometers; Assembly; Laser applications; Mirrors; Missiles; Power supplies; Ring lasers; Temperature distribution; Temperature sensors; Voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 1990. Record. The 1990's - A Decade of Excellence in the Navigation Sciences. IEEE PLANS '90., IEEE
Conference_Location
Las Vegas, NV
Type
conf
DOI
10.1109/PLANS.1990.66226
Filename
66226
Link To Document