发明名称 SPACE STABILIZER
摘要 PROBLEM TO BE SOLVED: To reduce the size of a space stabilizer by dismantling a triaxial optical fiber gyro into a plurality of components and fixing them to the inside/ outside of a housing section or a gimbal mechanism section. SOLUTION: In the space stabilizer, a plurality of components constituting each optical fiber gyro 10, 11, 13 are disposed at different positions, an optical component 26 to be connected with the optical fiber gyro 13 for detecting the roll axis is disposed at a position different from that of the optical fiber gyro 13 for detecting the roll axis in order to increase the degree of freedom of fixing while reducing the size.
申请公布号 JP2002062141(A) 申请公布日期 2002.02.28
申请号 JP20000247438 申请日期 2000.08.17
申请人 TAMAGAWA SEIKI CO LTD 发明人 ARAI AKIFUMI;KUBOTA AKIRA
分类号 F41G7/22;G01C19/00;G01C19/72;(IPC1-7):G01C19/72 主分类号 F41G7/22
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