发明名称 Compact, integral, 6-mirror, triaxial, laser rate gyro
摘要 A triaxial ring laser gyroscope with three square optical paths which are planar and orthogonal with respect to one another, this laser gyroscope comprising six optical mirrors interconnected two by two by means of twelve optical path segments (capillary channels), said segments forming an octahedron, with one mirror for each corner, each of the mirrors operating simultaneously in two orthogonal optical paths.
申请公布号 US4616929(A) 申请公布日期 1986.10.14
申请号 US19810252229 申请日期 1981.03.20
申请人 STE. FRANCAISE D'EQUIPEMENTS POUR LA NAVIGATION AERIENNE 发明人 BERNELIN, BERNARD;DE SALABERRY, BERNARD
分类号 G01C19/66;H01S3/083;(IPC1-7):G01C19/64;H01S3/101 主分类号 G01C19/66
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