Missile Attitude Safing System
Patent, Filed 28 Dec 64, patented 23 Mar 99
DEPARTMENT OF THE NAVY WASHINGTON DC
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An attitude sensing safing system for a missile, which senses an attitude error of the missile, and activates a dudding signal when the error exceeds a certain value for a predetermined time. The missile includes a delay arming timer, which is deactivated when by the dudding signal. The system allows the missile to correct itself, by requiring that the error signals persist for a set time.
- Guided Missile Warheads and Fuzes