• 제목/요약/키워드: Aerospace applications

검색결과 698건 처리시간 0.028초

VERIFICATION ON THE PERFORMANCE OF COMS SOC S-BANDSSPA

  • Park, Durk-Jong;Yang, Hyung-Mo;Ahn, Sang-Il
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.482-485
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    • 2007
  • The S-Band SSPA is front-end equipment to transmit both LRIT and HRIT to COMS. To provide the required EIRP, S-Band SSPA is designed to generate maximum 1kW power at its 1dB gain compression point (P1dB). Due to the operation for 24 hours per seven days, the verification on the performance of S-Band SSPA was performed thoroughly. This paper presents that major requirements such as maximum 1kW power, maximum -26dBc of IMD characteristic at 500W output and around -57dBc of coupling factor were verified through proposed test configuration.

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AN EXPERIMENTAL STUDY ON THE ESTABLISHMENT OF PRODUCT VALIDATION SITE AND THE RELATED ACTIVITIES

  • Lee Kwangjae;Kim Younsoo;Kim Yongseung;Hoersch Bianca
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.426-429
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    • 2005
  • In order to evaluate KOrea Multi-Purpose SATellite (KOMPSAT) application products and develop the multi-sensor data application technologies, the Product Validation Site (PVS) will be designed and constructed by Korea Aerospace Research Institute (KARI). Also KARl has a plan for acquisition of multi-sensor data such as ENVISAT ASAR and Project for On Board Autonomy (PROBA) Compact High Resolution Imaging Spectrometer (CHRIS) data through international cooperation with European Space Agency (ESA). These data will be utilized with KOMPSAT-2 Multi-Spectral Camera (MSC) data. KARI and ESA have identified a mutual interest in creating synergy in the joint exploitation of Earth Observation data for science and applications both in Korea and Europe. This paper summarizes the status of joint experimental studies between KARI and ESA for further applications and presents some expected results from related activities.

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On the Use of Finite Rotation Angles for Spacecraft Attitude Control

  • Kim, Chang Joo;Hur, Sung Wook;Ko, Joon Soo
    • International Journal of Aeronautical and Space Sciences
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    • 제18권2호
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    • pp.300-314
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    • 2017
  • This paper examines finite rotation angle (FRA) applications for spacecraft attitude control. The coordinate transformation matrix and the attitude kinematics represented by FRAs are introduced. The interpolation techniques for the angular orientations are thoroughly investigated using the FRAs and the results are compared to those using traditional methods. The paper proposes trajectory description techniques by using extremely smooth polynomial functions of time, which can describe point-to-point attitude maneuvers in a realizable and accurate manner with the help of unique FRA features. In addition, new controller design techniques using the FRAs are developed by combining the proposed interpolation techniques with a model predictive control framework. The proposed techniques are validated through their attitude control applications for an aggressive point-to-point maneuver. Conclusively, the FRAs provide much more flexibility than quaternions and Euler angles when describing kinematics, generating trajectories, and designing attitude controllers for spacecraft.

건전성예측 및 관리기술 연구동향 및 응용사례 (A review on prognostics and health management and its applications)

  • 최주호
    • 항공우주시스템공학회지
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    • 제8권4호
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    • pp.7-17
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    • 2014
  • Objective of this paper is to introduce a new technology known as prognostics and health management (PHM) which enables a real-time life prediction for safety critical systems under extreme loading conditions. In the PHM, Bayesian framework is employed to account for uncertainties and probabilities arising in the overall process including condition monitoring, fault severity estimation and failure predictions. Three applications - aircraft fuselage crack, gearbox spall and battery capacity degradation are taken to illustrate the approach, in which the life is predicted and validated by end-of-life results. The PHM technology may allow new maintenance strategy that achieves higher degree of safety while reducing the cost in effective manner.

항공우주용 소형 포펫 체크밸브 기술 동향 (Technology Trend of Small Poppet Type Check Valve for Aerospace Application)

  • 유재한;이수용
    • 항공우주산업기술동향
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    • 제9권1호
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    • pp.158-164
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    • 2011
  • 항공우주용으로 개발되거나 활용 가능한 상업용 체크밸브사례가 조사되었다. 개발사례로 발사체용, 높은 수명이 요구되는 NASA의 SSME (Space Shuttle Main Engine) 및 지상 지원 시스템 퍼지 라인용과 국내에서 개발된 체크밸브가 있다. 상용품은 미국 주요 밸브개발업체의 제품을 상온용과 극저온용으로 분류하여 조사하였다. 또한 운용 온도, 운용 압력 및 크래킹 압력과 같은 주요 성능과 관련된 씰의 재질, 스프링 강성과 같은 설계 인자의 관계도 설명되었다. 이러한 단품 성능 이외에 채터 및 오염과 같은 운용상의 문제점과 일반적인 해결방안도 언급되었다. 또한 기타주의사항으로 필터, 피팅과 청정도 요구조건에 대하여도 조사되었다

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차량 제어 기술 및 선진 연구 동향 (Vehicle Dynamics Control Applications to Automobiles: Survey and Some New Trends)

  • 이경수;이준영
    • 제어로봇시스템학회논문지
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    • 제20권3호
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    • pp.298-312
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    • 2014
  • This paper describes control applications in automobiles. Many aspects of automotive applications of advanced control methods, which include suspension systems, stability control systems, engines, hybrid vehicle control systems, electric vehicle controls systems, advanced driver assistance systems and automated driving control systems, are reviewed. The control methods used in each area are briefly reviewed to help readers understand the applicability and effectiveness of these methods. In addition, some new trends in the research of automotive applications are described.

NEW FRONTIERS IN THERMAL PLASMAS FROM SPACE TO NANOMATERIALS

  • Boulos, Maher I.
    • Nuclear Engineering and Technology
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    • 제44권1호
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    • pp.1-8
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    • 2012
  • Thermal plasma technology has been at the center of major developments over the past century. It has found numerous applications ranging from aerospace materials testing to nanopowder synthesis and processing. In the present review highlights of principal breakthroughs in this field are presented with emphasis on an analysis of the basic phenomena involved, and the potential of the technology for industrial scale applications.

하이브리드 쾌속 조형 시스템의 개발 및 나노 복합재 부품 제작 (Development of Hybrid RP System and Fabrication of Nano Composite parts)

  • 김성근;정우균;추원식;김형중;안성훈
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 추계학술대회 논문집
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    • pp.220-223
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    • 2005
  • The rapid prototyping (RP) technology has been advanced for various applications such as verification of design, functional test. However, many RP machines still have low accuracy and limitation of applications for various materials. In this research, a hybrid RP system was developed to improve precision of micro parts. This hybrid system consists of deposition and material removal process by mechanical micro machining to fabricate nano composites using photo-curable polymer resin with various nano particles. In this work, using hybrid RP process with Multi-Walled Carbon Nano Tube (MWCNT) and hydroxyapatite, micro parts were fabricated. The precision of parts was evaluated based on the original CAD design, and to see the effect of nano particles on mechanical properties, tensile strength was measured. From the results of experiments, it was confirmed that the part made by hybrid process had higher precision, and the addition of nano particles improved mechanical properties.

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Synthesis and Characterization of CrZr-O-N Films Using Cr-Zr Segment Targets by Unbalanced Magnetron Sputtering

  • Kim, Dong Jun;La, Joung Hyun;Ki, Sung Min;Lee, Sang Yul
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2013년도 제44회 동계 정기학술대회 초록집
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    • pp.94-94
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    • 2013
  • The Cr-Zr-N films have much improved mechanical properties and very smooth surface roughness. However, in spite of their outstanding properties, the Cr-Zr-N coatings revealed their mechanical properties deteriorated severely with increasing Zr content at $500^{\circ}C$ ecause of very rapid oxidation. Recently oxynitride films have been widely studied due to their excellent unique mechanical properties and oxidation resistance. In this work, CrZr-O-N films with various O contents were synthesized by unbalanced magnetron sputtering with Cr-Zr segment targets (Cr:Zr volume ratios is 1:1) and all films were prepared in a nitrogen rich mixture of N2 and O2. Characteristics such as crystalline structure, hardness and chemical composition as a function of the O content were investigated by X-ray diffraction (XRD), field emission scanning electron microscope (FE-SEM), microhardness testing system and energy dispersive spectroscopy (EDS). Results showed that the thin films had dense and compact microstructure as O content in the films increases. The microstructure of the thin films consisted of mainly crystalline Cr (Zr)N phase and Cr2O3 phase. The maximum hardness and elastic modulus of the films was measured to be approximately 33.2 GPa and 280.6 GPa from the films with low content of O elements. Detailed experimental results will be presented.

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