发明名称 DYNAMIC CALIBRATION RADAR SYSTEM
摘要 A missile radar system includes a tapered radome covering a front face of a main antenna. A calibration antenna is the combination of a metal tip and an attached one or more radiating or excitation elements (monopole) on the tip. A narrow end (wedge) of the radome may aid in directing planar calibration waves toward the main antenna. The metal tip has a curved inner surface that acts, with the attached radiating element(s), as an aperture antenna. Signals are emitted from the calibration antenna back toward the front face of the main antenna. The signals pass from the tip/reflector to the front face of the main antenna through a substantially-metal-free and substantially-dielectric-free volume defined by the inner surface of the radome. The radar system allows for calibration of the antenna prior to launch and/or during flight of the missile.
申请公布号 US2012249358(A1) 申请公布日期 2012.10.04
申请号 US201113076816 申请日期 2011.03.31
申请人 STRATIS GLAFKOS K.;SAMUEL ALPHONSO A.;BELLOFIORE SALVATORE;KNAPP DAVID J. 发明人 STRATIS GLAFKOS K.;SAMUEL ALPHONSO A.;BELLOFIORE SALVATORE;KNAPP DAVID J.
分类号 G01S13/00;G01S7/40 主分类号 G01S13/00
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