Solar panel is an important structure of the spacecraft, SADA (Solar Array Drive Assembly is often used as the drive organ to realize the step-skipped gesture adjustment. Firstly, the disturbance mechanism impact, which was produced from working SADA, to the electro-mechanism and payload coupling has been taken into account, and the dead, rigid and flexible load SADA disturbance model was established and validated through simulation and experimental measuring. Secondly, implemented the experimental check, calibration and correction to the mathematical model. Finally, the definition of electrical rigidity was proposed to analyze the disturbance mechanism of SADA, and verified its existence through simulation and testing.
목차
Abstract 1. Introduction 2. Analysis of the Principle of Solar Panel Driving Mechanism 3. Modeling of SADA Disturbance 3.1 The principles of producing SADA disturbance and electromagnetic rigidity 3.2 Dead load SADA model 3.3 Rigid load SADA model 3.4 Flexible load SADA model 4. SADA Simulation and Validation 5. SADA Disturbance Measuring Experiment 5.1 Dead load SADA experiment 5.2 Rigid load SADA experiment 5.3 Flexible load SADA experiment 6. Conclusion References
보안공학연구지원센터(IJHIT) [Science & Engineering Research Support Center, Republic of Korea(IJHIT)]
설립연도
2006
분야
공학>컴퓨터학
소개
1. 보안공학에 대한 각종 조사 및 연구
2. 보안공학에 대한 응용기술 연구 및 발표
3. 보안공학에 관한 각종 학술 발표회 및 전시회 개최
4. 보안공학 기술의 상호 협조 및 정보교환
5. 보안공학에 관한 표준화 사업 및 규격의 제정
6. 보안공학에 관한 산학연 협동의 증진
7. 국제적 학술 교류 및 기술 협력
8. 보안공학에 관한 논문지 발간
9. 기타 본 회 목적 달성에 필요한 사업
간행물
간행물명
International Journal of Hybrid Information Technology
간기
격월간
pISSN
1738-9968
수록기간
2008~2016
십진분류
KDC 505DDC 605
이 권호 내 다른 논문 / International Journal of Hybrid Information Technology Vol.7 No.2