发明名称 Device for measuring the heading error of a missile
摘要 A device for measuring the heading error of a missile, comprising two afocal systems for a taking-in-charge field PC and a cruising field CR, in front of a double prism, with a central prism and a peripheral prism of the same angle bonded together with their dihedrals opposed. The double prism is in front of a focusing lens in the focal plane of which are disposed four detectors. When one detector sees the PC field, the other detector sees the CR field. An analog switch permutes in a circular fashion a processing device to the PC channel or the CR channel, for delivering missile heading error measurement signals.
申请公布号 US4699332(A) 申请公布日期 1987.10.13
申请号 US19850732643 申请日期 1985.05.10
申请人 SOCIETE ANONYME DE TELECOMMUNICATIONS 发明人 BIGOT, GEORGES;LONNOY, JACQUES J.
分类号 F41G7/30;(IPC1-7):F41G7/26 主分类号 F41G7/30
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