A Study on the mixed mode of Gyro

자이로의 혼합모드 연구

  • 노영환 (우송대학교 컴퓨터전자정보공학부) ;
  • 방효충 (충남대학교 항공우주공학과) ;
  • 이상용 (우송대학교 컴퓨터전자정보공학부) ;
  • 황규진 (우송대학교 컴퓨터전자정보공학부)
  • Published : 2000.10.01

Abstract

In the three axis control of satellite by using reaction wheel and gyro, a Gyro carries out measuring of the attitude angie and the attitude angular velocity. The Gyro is operated by the electronic part and the mechanic actuator. The digital part of the electronic part is consisted of the FPGA (Field Programmable Gate Array), which is one of the methods for designing VLSI (Very Large Scale Integrated Circuit), and the mechanic actuator processes the input/output data by the dynamic model. In the research of the mixed mode of Gyro, the simulation is accomplished by SABER of the mixed mode simulator and the results for the practical implementation of the satellite ACS (Attitude Control System) interfaced with the data processing are proposed.

Keywords