发明名称 COMPOSITE SEEKER FOR MISSILE
摘要 <p>PURPOSE:To move a plurality of sensors by one spherical motor by providing a plurality of sensors for controlling to move a normal line of a spherical gimbal to be rotated by the motor. CONSTITUTION:When a relative distance between a target and a missile is reduced and becomes a distance for sufficiently aiming at the target even by an infrared ray sensor 4 for an optical wave seeker, the sensor 4 is switched from a radio wave antenna 3 for a radio wave seeker to an infrared ray sensor 4 for an optical wave seeker, and a guiding system is switched to an infrared ray tracing system having an excellent aiming accuracy. That is, a spherical gimbal 2 is rotated by a spherical motor, and a control shaft is switched from a gimbal control reference shaft 5 for the radio wave seeker to a gimbal control reference shaft 6 for the optical wave seeker. Thus, high accuracy tracing is again continued by controlling to rotate the gimbal 2. In this case, since the antenna 3 and the sensor 4 are mounted on a peripheral surface of a direction having a different bearing angle to an axis of the missile, sensing failure does not occur.</p>
申请公布号 JPH05196394(A) 申请公布日期 1993.08.06
申请号 JP19920008401 申请日期 1992.01.21
申请人 MITSUBISHI HEAVY IND LTD 发明人 NAKAJIMA HIROSHI
分类号 F41G7/22;F42B15/01;G01S13/88;G05D1/12 主分类号 F41G7/22
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