【摘要】 由三块反射镜组成的光学系统在轨道空间微重力的影响下,其反射镜面间隔、曲率半径往往发生改变,对系统的后截距产生较大的影响,最终导致相机离焦,成像质量下降。通过分析三反系统的等效高斯光学系统,得到其后截距公式;通过齐次坐标变换,得到反射镜面刚体位移公式;通过采用最小二乘算法拟合计算得到微重力环境下的镜面半径,计算出相机在空间环境下的离焦量为0.04 mm,为调焦机构的设计提供了理论依据。更多还原

【Abstract】 The mirror interval and radius of curvature of optical system including three mirrors are often changed due to the impact of space microgravity,which has a greater impact on the back focal length,and causes camera defocus and imaging quality reduction.Through the equivalent Gauss optical system analysis of three-mirror system,back focal length formula can be obtained.By homogeneous coordinate transformation,the reflection mirror rigid-body displacement formula is obtained,and a mirror radius is obtained in the microgravity environment using the least squares fitting algorithm.Finally,by calculating the camera in space microgravity environment,the defocusing amount is 0.04 mm.Results provide a theoretical basis for the design of focusing mechanism.更多还原