• The Science & Technology
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• no.10 s.461
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• pp.34-37
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• 2007

• Bulletin of the Korean Space Science Society
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• 2001.11a
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• pp.76-76
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• 2001

• Bulletin of the Korean Space Science Society
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• 2001.04a
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• pp.60-60
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• 2001

• Electrical & Electronic Materials
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• v.11 no.9
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• pp.48-54
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• 1998

• Bulletin of the Korean Space Science Society
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• 1999.04a
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• pp.11-11
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• 1999

• Bulletin of the Korean Space Science Society
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• 2002.05b
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• pp.60-60
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• 2002

• Superconductivity and Cryogenics
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• v.22 no.2
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• pp.2-7
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• 2020

• Journal of Satellite, Information and Communications
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• v.7 no.2
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• pp.72-75
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• 2012

A solar array makes a Solar Array Regulator (SAR) for Low-Earth-Orbit satellite have different small signal characteristic. Therefore, an Average-Current-Mode (ACM) controller cannot control the BUCK-BOOST type SAR which operates in a current region of the solar array. In this paper, we present the Pseudo-Continuous Current Mode (PCCM) BUCK-BOOST Type SAR which can be controller by the ACM Controller. We explain the circuit operation of the PCCM BUCK-BOOST Type SAR, derive its small signal transfer function and design ACM Controller. Finally, we verify the ACM control of the PCCM BUCK-BOOST Type SAR by using a simulation.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.9
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• pp.38-45
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• 2003

This research is concerned with the dynamic modeling of the multi-purpose satellite with deployable solar arrays equipped with strain energy hinges(SEH). To this end, we proposed the use of the equivalent torsional spring for the SEH and derived the equations of motion assuming that the satellite and solar arrays are being rigid. We also considered the effect of the support string for the ground experiment model, which has been observed as a critical factor affecting the deployment in the ground experiments. From the numerical simulation results, it is found that solar arrays are deployed in a similar pattern but the hub motions are different because of the support strings. It was concluded that the non-gravity deployment of the solar arrays can be approximately simulated by the ground experimental facility. The effects of the support string are also investigated by varying the length of the string. It was found that the current length of the string is adequate for the ground experiment. Ground experimental results will follow.

• Proceedings of the KIPE Conference
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• 2012.11a
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• pp.121-122
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• 2012

저궤도 인공위성의 전력변환 시스템은 태양전지판에서 생성된 전력을 배터리와 전장품으로 구성된 비조절형 버스로 전압 강하하여 제공한다. 무게, 부피, EMI/EMC 특성에 제한적인 요구조건을 갖는 인공위성의 응용분야에 적용하기 위하여 설계된 강압형 DC/DC 컨버터는 기존의 벅-컨버터와 유사한 동작특성을 보이지만 인턱터를 분리함으로써 입력단에도 연속적인 전류특성을 보이며 두 개로 분리된 인턱터는 부피와 무게에서 이점을 갖추고 있다. 본 논문에서는 연속적인 입출력 전류 특성을 갖는 강압형 컨버터의 동작특성에 대하여 기술한다.