• Journal of the Korean Society for Aviation and Aeronautics
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• v.14 no.1
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• pp.28-35
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• 2006

Substructure coupling or component mode synthesis may be employed in the solution of dynamic problems for large, flexible structures. The model is partitioned into several subdomains, and a generalized Craig-Bampton representation is derived. In this paper the mode sets (normal modes, constraint modes) is employed for model reduction. A generalized model reduction procedure is described. Vaious reduction methods that use constraint modes is described in detail. As examples, a flexible structure and a 10 DOF damped system are analyzed. Comparison with a conventional reduction method based on a complete model is made via eigenpair and dynamic responses.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2001.11b
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• pp.1370-1375
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• 2001

Substructure coupling or component mode synthesis may be employed in the solution of dynamic problems for structure. The model is partitioned into several subdomains. and a generalized Craig-Bampton representation is derived. In this paper the mode sets(normal modes. constraint modes) have been employed for model reduction. A generalized model reduction procedure has been described. Those reduction methods which adapt constraint modes have been described in detail. As examples. a flexible structure and a 10 DOF damped system are analyzed. Comparison with a conventional reduction method based on a complete model has been made via eigenpairs and dynamic responses.

• Proceedings of the KSRS Conference
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• 2009.03a
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• pp.78-81
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• 2009

레일형 GB-SAR의 단점을 극복하고자 차량에 원형레일을 탑재하여 신속한 기동을 확보하고 합성구경의 길이를 늘리며 영상영역을 확장한 ArcSAR를 세계 최초로 설계하고 시작품을 제작하였다. ArcSAR의 핵심기술이라고 할 수 있는 원형레일은 알루미늄 프로파일로 제작한 회전디스크, 곡선가이드, 리니어 가이드로 구성되며, 서보모터를 이용하여 구동된다. 회전디스크의 지름은 2.1 m 이며, 회전 디스크 위에 장착된 곡선 가이드를 따라 안테나가 탑재된 리니어 가이드가 이동하며 정밀한 원형 운행을 하게 된다. 리니어 가이드는 슬라이드식으로 제작되어 최대 3 m 까지 확장이 가능하여 스폿 모드 측정시 6 m 길이의 레일에서의 자료 획득과 유사한 결과를 얻게 된다. SAR 측정 장비는 회전디스크 위에 장착되어 전원을 제외한 별도의 슬립링을 사용을 자제하였다. 레일의 구동과 자료의 획득은 LabVIEW 기반의 통합 제어측정 소프트웨어를 통해 구현하였으며, 실내 실험 및 현장적용 실험을 통해 가능성을 확인하였다.

• Composites Research
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• v.37 no.3
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• pp.219-225
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• 2024

It is essential to develop a light-weight, high-performance structure for the deployable reflector antenna, which is the payload of a reconnaissance satellite, considering launch and orbital operation performance. Among them, the composite main reflector is a key component that constitutes a deployable reflector antenna. In particular, the development of a high-performance main reflector is required to acquire high-quality satellite images after agile attitude control maneuvers during satellite missions. To develop main reflector, the initial design of the main reflector was confirmed considering the structural performance according to the laminate stacking design and material properties of the composite main reflector that constitutes the deployable reflector antenna. Based on the initial design, four types of composite main reflectors were manufactured with the variable for manufacturing process. As variables for manufacturing process, the curing process of the composite structure, the application of adhesive film between the carbon fiber composite sheet and the honeycomb core, and the venting path inside the sandwich composite were selected. After manufacture main reflector, weight measurement, non-destructive testing(NDT), surface error measurement, and modal test were performed on the four types of main reflectors produced. By selecting a manufacturing process that does not apply adhesive film and includes venting path, for a composite main reflector with light weight and structural performance, we developed and verified a main reflector that can be applied to the SAR(Synthetic Aperture Rader) satellite.