Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1964-12-28
1999-03-23
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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.
Jordan Charles T.
Montgomery Christopher K
The United States of America as represented by the Secretary of
LandOfFree
Missile attitude safing system does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Missile attitude safing system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Missile attitude safing system will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2128508