• Title/Summary/Keyword: mirror mount

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Evaluation of a Aluminum Hyperbolic Mirror with the Diameter of 300 mm(f/1.98) by Using the Autostigmatic Null Lens System Assembled in a Fixed Tube Mount (경통고정식 자동무수차점 널 렌즈 테스트법을 이용한 직경 300 mm(f/1.98) 알루미늄 쌍곡면 거울의 형상측정)

  • Lee, Young-Hun;Jo, Jae-Heung;Rim, Cheon-Seog;Yang, Sun-Choel;Kim, Geon-Hee;Won, Jong-Ho;Jeong, Youn-Hong
    • Korean Journal of Optics and Photonics
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    • v.17 no.5
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    • pp.412-419
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    • 2006
  • We design and fabricate an autostigmatic null lens system assembled in a fixed tube mount in order to evaluate the shape of an aluminum hyperbolic mirror with the diameter of 300 mm and the f-number of 1.98, which is fabricated by a high precision aspherical DTM (diamond turning machine). Also, we evaluate the degree of shape of the aspherical mirror by this autostigmatic null lens testing method. The autostigmatic null lens system assembling in a fixed tube mount has several advantages of light weight, good mechanical stability, etc. The permissible fabricating limits of null lenses and a mount are determined by considering various tolerances to assure the measurement reliability.

Mirrors and Optomechanical Structures Design and Analysis for Linear Astigma-tism Free Three Mirror System (LAF-TMS)

  • Park, Woojin;Hammar, Arvid;Lee, Sunwoo;Chang, Seunghyuk;Kim, Sanghyuk;Jeong, Byeongjoon;Kim, Geon Hee;Kim, Daewook;Pak, Soojong
    • The Bulletin of The Korean Astronomical Society
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    • v.43 no.2
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    • pp.55.4-56
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    • 2018
  • Linear Astigmatism Free - Three Mirror System (LAF-TMS) is the linear astigmatism free off-axis wide field telescope with D = 150 mm, F/3.3, and $FOV=5.51^{\circ}{\times}4.13^{\circ}$. We report the design and analysis results of its mirrors and optomechanical structures. Tolerance allowance has been analyzed to the minimum mechanical tolerance of ${\pm}0.05mm$ that is reasonable tolerance for fabrication and optical alignment. The aluminum mirrors are designed with mounting flexure features for the strain-free mounting. From Finite Element Analysis (FEA) results of mounting torque and self-weight, we expect 33 - 80 nm RMS mirror surface deformations. Shims and the L-bracket are mounted between mirrors and the mirror mount for optical alignment. The mirror mount is designed with four light-weighted mechanical parts. It can stably and accurately fix mirrors, and it also suppresses some of stray light.

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Optomechanical Design and Structural Analysis of Linear Astigmatism Free - Three Mirror System Telescope for CubeSat and Unmanned Aerial Vehicle

  • Han, Jimin;Lee, Sunwoo;Park, Woojin;Moon, Bongkon;Kim, Geon Hee;Lee, Dae-Hee;Kim, Dae Wook;Pak, Soojong
    • The Bulletin of The Korean Astronomical Society
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    • v.46 no.1
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    • pp.38.3-38.3
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    • 2021
  • We are developing an optomechanical design of infrared telescope for the CubeSat and Unmanned Aerial Vehicle (UAV) which adapts the Linear Astigmatism Free- Three Mirror System in the confocal off-axis condition. The small entrance pupil (diameter of 40 mm) and the fast telescope (f-number of 1.9) can survey large areas. The telescope structure consists of three mirror modules and a sensor module, which are assembled on the base frame. The mirror structure has duplex layers to minimize a surface deformation and physical size of a mirror mount. All the optomechanical parts and three freeform mirrors are made from the same material, i.e., aluminum 6061-T6. The Coefficient of Thermal Expansion matching single material structure makes the imaging performance to be independent of the thermal expansion. We investigated structural characteristics against external loads through Finite Element Analysis. We confirmed the mirror surface distortion by the gravity and screw tightening, and the overall contraction/expansion following the external temperature environment change (from -30℃ to +30℃).

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Pointing Accuracy Analysis of Space Object Laser Tracking System at Geochang Observatory (거창 우주물체 레이저 추적 시스템의 추적마운트 지향 정밀도 분석)

  • Sung, Ki-Pyoung;Lim, Hyung-Chul;Park, Jong-Uk;Choi, Man-Soo;Yu, Sung-Yeol;Park, Eun-Seo;Ryou, Jae-Cheol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.11
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    • pp.953-960
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    • 2021
  • Korea Astronomy and Space Science Institute has been verifying the multipurpose laser tracking system with three functions of satellite laser tracking, adaptive optics and space debris laser tracking for not only scientific research but also national space missions. The system employs an optical telescope consisting of a 100 cm primary mirror and an altazimuth mount for fast and precise tracking. The precise pointing and tracking capability in a tracking mount is considered as one of important performance metrics in the fields of automatic tracking and precise application research. So it is required to analyze a mount model for investigating pointing error factors and compensating pointing error. In this study, we investigated various factors causing static pointing errors of tracking mount and analyzed the pointing accuracy of the tracking mount at Geochang observatory by estimating mount parameters based on the least square method.

Optical Design for UVOMPIS and Design Concept of the Mirror Holder

  • Park, Woojin;Chang, Seunghyuk;Pak, Soojong;Han, Jimin;Ahn, Hojae;Lee, Sunwoo;Kim, Geon Hee;Lee, Dae-Hee
    • The Bulletin of The Korean Astronomical Society
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    • v.45 no.1
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    • pp.66.3-66.3
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    • 2020
  • We present the optical design of Linear Astigmatism Free - Three Mirror System (LAF-TMS) D200 for UVO-Multiband Polarizing Imager System (UVOMPIS). LAF-TMS D200 is the off-axis wide-field telescope with EPD = 200 mm, F/2, and Field of View (FoV) = 2° × 4°. Its optical mirrors are optimized to freeform surfaces for high-quality optical performance over a wide FoV. The proposed mirror holder consists of four aluminum optomechanical modules that have applied for LAF-TMS D150 which is a prototype of the LAF-TMS system. It can accurately mount mirrors and also can sustain from vibration environments. As a feasibility study, quasi-static, modal, harmonic, and random vibration analyses have been performed to LAF-TMS D150 optomechanical structure under the qualification level of the Soyuz-2/Fregat launch system. We evaluate the vibration analysis results in terms of von Mises stress and Margin of Safety.

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IGRINS : Collimating Mirror Mount Opto-mechanical Design

  • Rukdee, Surangkhana;Park, Chan;Chun, Moo-Young;Yuk, In-Soo;Lee, Sung-Ho;Lee, Han-Shin;Kim, Kang-Min;Jeong, Hwa-Kyung;Strubhar, Joseph;Jaffe, Daniel T.
    • Bulletin of the Korean Space Science Society
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    • 2011.04a
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    • pp.30.4-31
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    • 2011
  • The Korea Astronomy and Space Science Institute (KASI) and the Department of Astronomy at the University of Texas at Austin (UT) are developing a near infrared wide-band high resolution spectrograph, IGRINS (Immersion Grating Infrared Spectrograph). The white-pupil design of the instrument optics uses 7 cryogenic mirrors including 3 aspherical off-axis collimators and 4 flat fold mirrors. Two of the 3 collimators are H- and K-band pupil transfer mirrors and they are designed as compensators for the system alignment in each channel. Therefore, their mount design will be one of the most sensitive parts in the IGRINS optomechanical system. The design work will include the computer-aided 3D modeling and finite element analysis (FEA) to optimize the structural stability of the mount models. The mount body will also include a tip-tilt and translation adjustment mechanism to be used as the alignment compensators.

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IGRINS : Mirror Mounts Optomechanical Design

  • Rukdee, Surangkhana;Park, Chan;Lee, Sung-Ho;Jaffe, Daniel T.;Lee, Han-Shin;Oh, Hee-Young;Jung, Hwa-Kyung;Yuk, In-Soo;Strubhar, Joseph;Kim, Kang-Min;Chun, Moo-Young
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.155.1-155.1
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    • 2011
  • The Korea Astronomy and Space Science Institute (KASI) and the Department of Astronomy at the University of Texas at Austin (UT) are developing a near infrared wide-band high resolution spectrograph, IGRINS (Immersion Grating Infrared Spectrograph). The white-pupil design of the instrument optics uses 7 cryogenic mirrors including 3 aspherical off-axis collimators and 4 flat fold mirrors. Two of the 3 collimators are H- and K-band pupil transfer mirrors and they are designed as compensators for the system alignment in each channel. Therefore, their mount design will be one of the most sensitive parts in the IGRINS optomechanical system. The other flat fold mirrors are designed within the limited area. Each of those includes the features of 3 axial hard points and 2 radial hard points with one spring plunger in order for the proper deflection of the mirror. The design work will include the computer-aided 3D modeling and finite element analysis (FEA) to optimize the structural stability and the thermal behavior of the mount models. The mount body will also include a tip-tilt and translation adjustment mechanism to be used as the alignment compensators.

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Improved kinematic mount design for bar type reference mirror for profilometric measurement large optical surface

  • Jung, Kil-Jae;Yang, Ho-Soon;Rhee, Hyug-Gyo;Jyun, Byoung-Hyug;Lee, Yun-Woo;Kim, Sug-Whan
    • Bulletin of the Korean Space Science Society
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    • 2010.04a
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    • pp.25.3-25.3
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    • 2010
  • Our previous study used a bar-type reference mirror to measure the relative distance to the target surface. The target measurement accuracy was required to $1{\mu}m$ PV for aspheric optical surface up to 1m in diameter. Earlier system suffers from the reference surface deformation when the measuring part moves. In order to reduce the deformation, measuring part and the reference part separated from each order in the new design. This system utilizes a kinematic support assembly using invar flexure to minimize the reference surface deformation under gravity and vibration. The surface deformation requirement of reference mirror is defined as of $0.2{\mu}m$ under gravity and 40Hz vibration. The finite element results, shows reference mirror deformation of $0.164{\mu}m$. The first resonance mode was computed to analysis 46.05Hz for reference part and 43.44Hz for measuring part. Thesis satisfies the frequency requirement.

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Range finding algorithm of equidistance stereo catadioptric mirror (등거리 스테레오 전방위 렌즈 영상에 대한 위치 측정 알고리즘)

  • Choi, Young-Ho
    • Journal of Internet Computing and Services
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    • v.6 no.6
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    • pp.149-161
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    • 2005
  • Catadioptric mirrors are widely used in automatic surveillance system. The major drawback of catadioptric mirror is its unequal image resolution. Equidistance catadioptric mirror can be the solution to this problem. Even double panoramic structure can generate stereo images with single camera system. So two images obtained from double panoramic equidistance catadioptric mirror can be used in finding the depth and height values of object's points. But compared to the single catadioptric mirror. the image size of double panoramic system is relatively small. This leads to the severe accuracy problem in estimation. The exact axial alignment and the exact mount of mirror are the sources that can be avoided but the focal length variation is inevitable. In this paper, the effects of focal length variation on the computation of depth and height of object' point are explained and the effective focal length finding algorithm, using the assumption that the object's viewing angles are almost same in stereo images, is presented.

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