Monitoring Safety System
Patent, filed 26 Jul 65, patented 23 Mar 99
DEPARTMENT OF THE NAVY WASHINGTON DC
Pagination or Media Count:
The invention pertains to a guidance monitoring safety system for a guided missile having platform gyros and electromechanical integrators with inputs from a guidance information analyzer. The system monitors malfunctions resulting from erratic or unsafe missile flight either the missile if any malfunctions are present or providing a safe-to-arm fuzing signal in the absence of malfunctions.
- Guided Missiles
- Ammunition and Explosives