A Review of EOS Thermal Control Logic for MSC on KOMPSAT-2

  • Heo H.P. (Korea Aerospace Research Institute) ;
  • Kong J.P. (Korea Aerospace Research Institute) ;
  • Kim Y.S. (Korea Aerospace Research Institute) ;
  • Park J.E. (Korea Aerospace Research Institute) ;
  • Youn H.S. (Korea Aerospace Research Institute) ;
  • Paik H.Y. (Korea Aerospace Research Institute)
  • 발행 : 2004.10.01

초록

MSC (Multi-Spectral Camera) system is a remote sensing instrument to obtain high resolution ground image. EOS (Electro-Optic System) for MSC mainly consists of PMA (Primary Mirror Assembly), SMA (Secondary Mirror Assembly), HSTS (High Stability Telescope Structure) and DFPA (Detector Focal Plane Assembly). High performance of EOS makes it possible for MSC system to provide high resolution and high quality ground images. Temperature of the EOS needs to be controlled to be in a specific range in order not to have any thermal distortion which can cause performance degradation. It is controlled by full redundant CPU based electronics. The validity of thermistor readings can be checked because a few thermistors are installed on each control point on EOS. Various kinds of thermal control logics are used to prevent 'Single Point Failure'. Control logic has a few set of database in order not to be corrupted by SEU (Single Event Upset). Even though the thermal control logic is working automatically, it can also be monitored and controlled by ground-station operator. In this paper, various ways of thermal control logic for EOS in MSC will be presented, which include thermal control mode and logic, redundancy design and status monitoring and reporting scheme.

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