Synthetic array radar command air launched missile system

Communications: radio wave antennas – Antennas – Balanced doublet - centerfed

Patent

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343 5CM, 343 16M, G01S 902

Patent

active

042042100

ABSTRACT:
A missile guidance system in which a synthetic array radar antenna control system correlates the phase and doppler frequency information contained in signals received by a four quadrant antenna from an illuminated section of terrain, so as to compute the velocity components of the antenna. The velocity components are utilized, in conjunction with the earth rate supplied from a terrestrial navigation system, to maintain the azimuth null plane of the antenna in alignment with a selected target designated by means of a synthetic array map of the illuminated terrain. A missile command system controls the flight path of missile along the azimuth null plane to the target.

REFERENCES:
patent: 3201788 (1965-08-01), Hertwig
patent: 3307179 (1967-02-01), Verbarg
patent: 3579239 (1971-05-01), Porcell, Jr. et al.
patent: 3631485 (1971-12-01), Beazell, Jr.
patent: 3774202 (1973-11-01), Nolette
patent: 3848253 (1974-11-01), Genuist et al.

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