$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

논문 상세정보

Abstract

The Electric Power Subsystem (EPS) is one of the most critical systems on any satellite because nearly every subsystem requires power. This makes the choice of power systems the most important task facing satellite designers. The main purpose of the Satellite EPS is to provide continuous, regulated and conditioned power to all the satellite subsystems. It has to withstand radiation, thermal cycling and vacuums in hostile space environments, as well as subsystem degradation over time. The EPS power characteristics are determined by both the parameters of the system itself and by the satellite orbit. After satellite separation from the launch vehicle (LV) to its orbit, in almost all situations, the satellite subsystems (attitude determination and control, communication and onboard computer and data handling (OBC&DH)), take their needed power from a storage battery (SB) and solar arrays (SA) besides the consumed power in the EPS management device. At this point (separation point, detumbling mode), the satellite's angular motion is high and the orientation of the solar arrays, with respect to the Sun, will change in a non-uniform way, so the amount of power generated by the solar arrays will be affected. The objective of this research is to select satellite EPS component types, to estimate solar array illumination parameters and to determine the efficiency of solar arrays during both detumbling and normal operation modes.

참고문헌 (14)

  1. Wertz, J. and Larson, W., Eds., Space Mission Analysis and Design. Boston, Kluwer Academic Publishers, 1991 
  2. You zheng, Gong ke, 'Tsinghua Micro/Nanosatellite research and it's application', 13th Annual AIAA/USU Conference on Small Satellites, SSC99-IX-3 
  3. Greg Merritt and John Opiela, 'Satellite Power Systems Sizing', www.tsgs.utexas/tadp/1995/spects/power 
  4. James R. Wertz, editor. Spacecraft Attitude Determination and Control. Kluwer Academic Publishers, Dordrecht, 2000 
  5. Peter C. Hughes. Spacecraft Attitude Dynamics. John Wiley and Sons, New York, 1986 
  6. Paul E. Panneton and Jason E. Jenkins, 'The MSX Spacecraft Power Subsystem', Johns Hopkins APL Technical Digest, Volume 17, Number 1 (1996) 
  7. Masoum, Mohamed A.S. and Dehbonei, Hooman, 'Design, Construction and Testing of a Voltage-based Maximum Power Point Tracker (VMPPT) for Small Satellite Power Supply', 13th Annual AIAA/USU Conference on Small Satellites, SSC99-XII-7 
  8. ManTech for Multi-Junction Solar Cells, http://www.afrl.af.mil/techconn/index.htm 
  9. S.R. Cvetkovic and G.J. Robertson, 'Spacecraft Design Considerations for Small Satellite Remote Sensing', IEEE Transaction on Aerospace and Electronic Systems, Vol. 29, No. 2, April 1993 
  10. TERMA A/S Space Division, 'Power Management and distribution Systems', www.terma.com 
  11. Spectrolab Inc. 12500 Gladstone Avenue, Sylmar, California 91342 USA, www.spectrolab.com 
  12. D. A. Vallado, Fundamentals of Astrodynamics and Applications. NY: McGraw-Hill, 1997 
  13. Andy Bradford, Luis M Gomes, Prof. Sir Martin Sweeting and Gokhan Yuksel, Cem Ozkaptan, Unsal Orlu, 'BILSAT-1: A Low-Cost, AGILE, Eearth Observation Microsatellite for TURKEY', 53rd International Astronautical Congress October 2002/Houston, Texas 
  14. D.G. Belov, et.al, 'Electric Power Supply for Ocean Satellite', sixth European Space Power Conference, Porto, Portugal, 6-10 May 2002 (ESA SP-502, May 2002) 

이 논문을 인용한 문헌 (2)

  1. 2009. "" Journal of power electronics : JPE, 9(4): 631~642 
  2. 2009. "" Journal of power electronics : JPE, 9(5): 679~690 

원문보기

원문 PDF 다운로드

  • ScienceON :

원문 URL 링크

원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다. (원문복사서비스 안내 바로 가기)

상세조회 0건 원문조회 0건

DOI 인용 스타일