Missile attitude safing system

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

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Details

102264, 102206, 102215, F42C 1106, F42C 1544

Patent

active

058863397

ABSTRACT:
An attitude sensing safing system for a missile, which senses an attitude ror 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.

REFERENCES:
patent: 3073550 (1963-01-01), Young
patent: 3086468 (1963-04-01), Mountjoy et al.

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