원문정보
보안공학연구지원센터(IJHIT)
International Journal of Hybrid Information Technology
Vol.7 No.2
2014.03
pp.123-138
피인용수 : 0건 (자료제공 : 네이버학술정보)
초록
영어
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
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
저자정보
참고문헌
자료제공 : 네이버학술정보