References
- 인공 위성용 태양센서의 제작에 관한 연구 옥건호
- SOLAR CELLS Green, M. A.
- Spacecraft Dynamics and Control Sidi, M. J.
- Spacecraft Attitude Determination and Control Wertz, J. R.
PSS(Pyramidal type 2-axes Analog Sun Sensor) which will be used for KAISTSAT-4 is designed to be small, light, low in power consumptions, and adequate for small satellite attitude sensor. The PSS for the KAISTSAT-4 consists of the pyramidal structure, solar cells and amplifier. The pyramidal structure is suitable for the 2-axes sensing, Solar cells are made up of a rectangular shape of crystal silicon. The PSS measures the angle of incident light and initial satellite attitude measurement, and provides an alarm for the sunlight-sensitive payloads. This paper explains the PSS structure and the characteristic test result about the PSS with