MISSILE ATTITUDE SAFING SYSTEM
Assignee
Filed
Jan 22, 1982
Granted
Mar 23, 1999
Location
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.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 22, 1982
Rescinded
Nov 3, 1998
Duration
16 years, 9 months
Record Details
- Patent number
- US 5886339
- Application
- 04423641
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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