Pseudo GPS aided multiple projectile bistatic guidance

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

Reexamination Certificate

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Details

C244S003100, C244S003110, C701S001000, C701S002000, C701S003000, C701S207000, C701S213000, C342S042000, C342S043000, C342S061000, C342S062000, C342S175000, C342S195000

Reexamination Certificate

active

07121502

ABSTRACT:
A guidance system for guiding each of several projectiles toward a moving target has a platform having a radar system for illuminating the target with a radar signal. Each projectile has a receiver for receiving the radar signal reflected from the target, a transponder for replying to Global Positioning System (GPS) like timing signals from several timing signal sources, and a data link transceiver for establishing a bidirectional data link to the platform. The data link carries the measured frequency shift of the radar signal reflected from the target as measured by the projectile. A computer on the platform computes a relative position of each projectile with respect to the target from tracking the moving target using the radar system and the reply signal from the transponder on each projectile. The data link sends guidance commands from the platform to each projectile to guide the projectile to the target.

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