发明名称 GUIDANCE SYSTEM FOR FLYING OBJECT
摘要 PURPOSE: To eliminate any necessity of a complicated ginbal mechanism so as to perform accurate guidance without any erroneous action by controlling read-out of data from a galvano-mirror, a polygon mirror, and a memory circuit which are scanners in an image pickup part without mounted on the ginbal of the image pickup part. CONSTITUTION: When flight of a flying object 21 is started, visual sight in the flying direction is secured by an objective lens 22 for combinedly used as a dome and this passes through a relay lens 23 so as to be parallel incident on a galvano-mirror 24. As for the visual light which is incident on the mirror 24, only the part where a necessary target is positioned among the vertical visual sight angle is scanned by strap calculation of a strap calculation circuit 30. Secondarily, it is incident on a polygon mirror 25, is incident on a radar 27 via an image formation lens 26, and an image signal is generated. The image signal is stored in a memory circuit 28, the image data of a part where a necessary target is positioned among the lateral visual sight is read by the circuit 30 and the image specified its visual sight in the vertical and lateral direction is provided.
申请公布号 JPH08166211(A) 申请公布日期 1996.06.25
申请号 JP19940332590 申请日期 1994.12.13
申请人 TECH RES & DEV INST OF JAPAN DEF AGENCY;KAWASAKI HEAVY IND LTD 发明人 MIZUTA TOSHIYA;AKIYAMA AKIRA;NISHIDA YOSHIHIKO;INOTSUME TAKAHIRO;SASAKI YASUHIKO
分类号 F41G7/22;F42B15/01;G01B11/00;G01S3/782;G02B26/10;G02B26/12;H04N7/18;(IPC1-7):G01B11/00 主分类号 F41G7/22
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