• Title/Summary/Keyword: 고속 스티어링 미러

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Design of the Step-stare Image Gathering System for an Aerial Reconnaissance (항공 정찰용 Step-stare 영상획득 시스템 설계)

  • Baek, Woonhyuk;Park, Jaeyoung;Ahn, Junghun;Lee, Jungsuk
    • Journal of the Korean Society for Precision Engineering
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    • v.31 no.9
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    • pp.813-820
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    • 2014
  • This paper presents design and performance validation of a method for motion compensation using fast steering mirror. First of all, the schematics of the Electro Optical/Infra-Red (EO/IR) and step-stare image gathering system for an aerial reconnaissance are introduced. Because of the steering mirror with low inertia so called Back scan mechanism (BSM), the fast step-stare image gathering technique that is required for taking a high-definition still image will be realized. After then, the BSM hardware includes motors and feedback sensors are introduced. Also, the motion profile for BSM will be designed to compensate roll scan motion of the gimbals. At the end of this paper, designed profile and tracking performance of the EO/IR system with BSM will be validated through experiments.

Performance Evaluation of the Tip-tilt Actuator in Fast Steering Secondary Mirror for Large Telescope (대형 망원경용 FSM(Fast Steering Secondary Mirror)을 위한 팁틸트 액츄에이터의 성능평가)

  • Kim, Ho Sang;Lee, Dong-Chan;Lee, Kyoung-Don;Kim, Young-Soo
    • Journal of the Korean Society for Precision Engineering
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    • v.31 no.5
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    • pp.403-409
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    • 2014
  • For ground-based telescope application, the performance assessment of tip-tilt actuator is important because the optical quality of telescope depends upon the windshake compensation ability of the fast steering secondary mirror. But it is difficult to measure the performance characteristics of the actuators due to the large size mirror and test facilities including the vacuum support and structural frame. In this paper, the full-scale tip-tilt test bed for the large size secondary mirror with diameter of 1m is built and the several tests are performed including the range, resolution and frequency response function. From the measurement results, it is shown that the tip-tilt actuator can successfully compensate the windshake with frequency of maximum 12 Hz and be a candidate for the Giant Magellan Telescope.