초록 ▼

A munition is presented which includes an integrity verification system that measures the integrity of the munition. When an integrity threshold is not met, engagement of the munition with a predetermined target is aborted. Also presented is a methodology for gating the engagement of the munition wi

A munition is presented which includes an integrity verification system that measures the integrity of the munition. When an integrity threshold is not met, engagement of the munition with a predetermined target is aborted. Also presented is a methodology for gating the engagement of the munition with the target. The methodology includes performing an integrity check of the munition after it is deployed. The method further includes aborting the engagement of the target when the integrity check of the munition fails.

대표청구항 ▼

What is claimed is: 1. A method comprising: deploying a munition to engage a target, the munition including a guidance system; performing an integrity check of the munition, performing the integrity check comprising determining if the munition will not engage the target beyond an alert limit; and i

What is claimed is: 1. A method comprising: deploying a munition to engage a target, the munition including a guidance system; performing an integrity check of the munition, performing the integrity check comprising determining if the munition will not engage the target beyond an alert limit; and if the integrity check fails, aborting the engagement of the target with the munition, wherein aborting the engagement of the target includes determining if an integrity error is recoverable and when the error is recoverable then not aborting the engagement of the munition with the target, and when the integrity error is not ercoverable then aborting the engagement of the munition with the target. 2. The method of claim 1 wherein deploying a munition comprises deploying a precision guided missile (PGM). 3. The method of claim 1 wherein deploying a munition comprises deploying a munition having a Global Positioning System (GPS) guidance system adapted to receive signals from a Space Base Augmentation System (SBAS). 4. The method of claim 1 wherein aborting comprises performing one of the group consisting of self-destructing the munition, diverting the munition to a predetermined location, disarming the munition, and failing to arm the munition. 5. The method of claim 1 wherein performing the integrity check comprises performing the integrity check a plurality of times between the time the munition is deployed and a time before the munition engages the target. 6. The method of claim 1 wherein performing the integrity check comprises performing an integrity check at a rate selected from the group consisting of continuously, at predetermined intervals, and on an interrupt basis. 7. The method of claim 1 wherein performing the integrity check comprises performing a final integrity check before the munition reaches a point of no return. 8. The method of claim 7 wherein aborting the engagement of the target comprises performing one of the group consisting of self-destructing the munition, diverting the munition to a predetermined location, disarming the munition, and failing to arm the munition.