发明名称 LAZER MISSILE SEEKER DEVICE ADAPTING CDL
摘要 PROBLEM TO BE SOLVED: To provide a missile seeker device to detect wind generated by a helicopter hiding out in a recess of a mountain by a coherent Doppler LIDAR system and generate an induction signal induced thereto. SOLUTION: A missile seeker device comprises laser irradiation parts 16, 11, 12, and 13 to perform irradiation with laser, laser receiving parts 13, 12, 15, and 17 to receive a reflection wave by pointing to the same direction as that of an optical axis of irradiation and output an output signal based on the reflection wave, a detector 17 to detect the presence of an object based on a detected Doppler frequency by varying a frequency band by discriminating the frequencies of output signals from the laser receiving parts, and a LIDAR signal processing part 18 to output an induction signal related to the flying direction of a missile based on the detecting result. A turbulent flow of the atmosphere by a helicopter is detected by a coherent Doppler LIDAR system to induce a flying object.
申请公布号 JP2001263994(A) 申请公布日期 2001.09.26
申请号 JP20000080950 申请日期 2000.03.22
申请人 TOSHIBA CORP 发明人 AYABE KOSUKE;CHIBA MASAAKI
分类号 F41G7/26;F41G7/20;G01S17/10;G01S17/66;(IPC1-7):F41G7/26 主分类号 F41G7/26
代理机构 代理人
主权项
地址