摘要
介绍了用于卫星姿态控制的太阳敏感器地面模拟试验与标定的空间小型太阳模拟器的结构设计方案。由光源发出的光经模拟器本体底部发出照射到待标定的工作面,通过步进电机控制模拟器的转动来实现入射光角度的变化。从而模拟太阳相对于太阳敏感器的矢量方位角的变化。
This paper introduces the structural design of small-scale spatial solar simulator which calibrating and ground simulation testing the solar sensor that used in satellite attitude control.The light of the simulator through the bottom irradiate the face of the object under test,through stepper motor to control the simulator to achieve the angle change of the incident light.Thus simulates the vector azimuth change the sun relative to the solar sensor.
出处
《长春理工大学学报（自然科学版）》
2010年第4期28-30,共3页
Journal of Changchun University of Science and Technology(Natural Science Edition)
