Geographically limited missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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Details

342357, 244 315, F41G 728

Patent

active

061424110

ABSTRACT:
A self destruct mechanism for an airborne projectile is provided. The projectile includes a navigation system which provides an absolute global position of the projectile. The position is compared with positions stored in memory. If the position of the projectile is determined to be acceptable, operation of the projectile continues. If the position of the projectile is unacceptable, an electronic control system initiates a self-destruct signal for the projectile.

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