| 摘要 |
PROBLEM TO BE SOLVED: To realize high observation accuracy by realizing high geometric accuracy without being affected in posture variation of a missile. SOLUTION: A component box 16 wherein a sensor body 18 is contained and arranged is connected with freedom in three dimensional directions to a space ship body 10 by way of joint mechanisms 15 and 17 and connection member 14, and electrically connected to each other by way of a transmission path 20 to constitute so that the posture of the component box 16 in inertial space is controlled independently of the space ship body 10.
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