大口径超宽幅空间相机装调支撑结构设计与仿真分析OA
Design and Simulation Analysis of Assembly and Adjustment Support Structure for Large-aperture Ultra-wide Format Space Camera
大尺寸空间光学相机在地面装调时存在的结构应力过大,支撑点受力状态无法准确测量,因此导致相机重力变形无法补偿、装调状态与在轨成像状态不一致,为解决此技术难题.以某3m级离轴三反超宽幅空间相机为例,提出了高精度装配支撑工装的方案设计与仿真分析.为满足地面与在轨成像条件,采用三点完全约束原理,利用"Kelvin clamp"支撑方式,有效降低了地面装调过程中产生的连接应力.为保证装调精度,该工装通过压力传感器实时采集装调工装支撑点压力数据,结合主动调节螺母对单点压力实时动态调整,确保了装调过程与有限元仿真相机的受力状态保持高度一致.在此基础上,借助Hypermesh建立整机有限元模型,对比分析支撑工装优化前后各反射镜RMS值及刚体位移值,通过Zemax软件完成相机光学指标的校核工作.有限元仿真与实测数据表明,该支撑结构可将各反射镜面形的RMS值控制在0.02λ以下.通过引入主动受力调节机制,M1、M3和M4反射镜的重力变形得到有效控制.此支撑结构能够解决大尺寸空间相机在地面装调过程中应力控制和重力补偿的难题,为同类型高分辨率空间相机的地面装调工作提供了有价值的技术支持.
To solve the technical problems existing in the ground assembly and alignment of large-scale space optical cameras,including excessive structural stress,inaccurate measurement of the force state at support points,as well as the consequent inability to compensate for camera gravity-induced deformation and the inconsistency between the assembly-alignment state and the on-orbit imaging state.Taking a 3-meter-class off-axis three-mirror anastigmat(TMA)ultra-wide-format space camera as an example,the scheme design and simulation analysis of a high-precision assembly support fixture is presented.To meet the ground and on-orbit imaging conditions,the three-point full constraint principle is adopted,and the"Kelvin clamp"support method is utilized to effectively reduce the connection stress generated during the ground assembly and alignment process.To ensure the assembly and alignment accuracy,the fixture collects the pressure data of the support points of the assembly fixture in real time through pressure sensors,and realizes real-time dynamic adjustment of the single-point pressure in combination with active adjustment nuts,ensuring that the force state of the camera during the assembly and alignment process is highly consistent with that of the finite element simulation.On this basis,a full-machine finite element model is established with Hypermesh to compare and analyze the RMS values and rigid body displacement values of each mirror before and after the optimization of the support fixture,and the verification of the camera's optical indicators is completed through Zemax software.Finite element simulation and measured data show that the support structure can control the RMS value of the surface shape of each mirror below 0.02λ.By introducing an active force adjustment mechanism,the gravity-induced deformation of the M1,M3 and M4 mirrors is effectively controlled.The problems of stress control and gravity compensation in the ground assembly and alignment of large-scale space optical cameras are solved by this support structure,and valuable technical support is provided for the ground assembly and alignment of similar high-resolution space optical cameras.
李淼;冯钧;赵桐;李小冬;隋鑫禹;于洋
中国科学院 长春光学精密机械与物理研究所,长春 130033中国科学院 长春光学精密机械与物理研究所,长春 130033中国科学院 长春光学精密机械与物理研究所,长春 130033中国科学院 长春光学精密机械与物理研究所,长春 130033中国科学院 长春光学精密机械与物理研究所,长春 130033中国科学院 长春光学精密机械与物理研究所,长春 130033
机械制造
空间相机装调工装Kelvin clamp有限元分析光学装调
space cameraassembly toolingKelvin clampfinite element analysisoptical alignment
《机电工程技术》 2026 (10)
39-44,6
吉林省自然科学基金-面上项目(20250102177JC)
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