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描述了东方红三号卫星 (DFH - 3)控制系统设计和数学仿真中采用的摆动扫描地球敏感器IRES - 0 1的数学模型 ,东方红三号卫星近三年飞行试验结果与数学仿真结果基本一致 ,证明数学模型是正确的
The mathematic model of the oscillating scanning earth sensor IRES - 0 1 used in DFH - 3 control system design and mathematical simulation is described. The flight test results and mathematical simulation results of Dongfanghong 3 satellite in recent three years Consistent, prove the mathematical model is correct