发明名称 SEMIACTIVE LASER GUIDE SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a semiactive laser guide system, improving the hitting accuracy of an airframe and extending a target detecting distance without any increase in size of the system. SOLUTION: In this semiactive laser guide system, a laser beam Lp from a laser irradiation means 1 is applied to the target X, the reflected light Lr reflected on the target X is detected to compute a target angle of the target X, and the airframe is guided and controlled according to the target angle. The laser irradiation means 1 includes a modulating function of scanning an irradiating laser beam Lp to the target X and changing the pulse cycle of the laser beam Lp corresponding to the scanning angle, and the airframe 10 includes a function of recognizing a scanning angle from the pulse cycle obtained by demodulating the detected reflected light Lr, and obtaining a correction angle from the scanning angle to correct an incident angle of reflected light detected and obtain a target angle to the target X. COPYRIGHT: (C)2009,JPO&INPIT
申请公布号 JP2009210175(A) 申请公布日期 2009.09.17
申请号 JP20080052857 申请日期 2008.03.04
申请人 NEC CORP 发明人 SAKAMOTO KENICHI
分类号 F41G7/22 主分类号 F41G7/22
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