| 摘要: |
| 针对航天伺服系统现有设计过程中因设计参数耦合因素考虑不全导致系统性能难以进一步提高的问题，提出了一套模块化航天机电伺服系统多学科集成设计与优化方法。从产品层、部件层和零件层对系统进行了模块化划分，给出了模块化设计流程及V字数据传递路线，以具体工程实例验证了模块化集成设计与优化方法的高效性及提升航天伺服系统总体设计水平的可行性。 |
| 关键词: 航天伺服系统 多学科集成设计 模块化设计 |
| DOI： |
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| 基金项目: |
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| Multidisciplinary Integrated Design and Optimization for Modular Aerospace Electromechanical Actuator |
| JIANG Menglong,AN Linxue,ZHU Yangzhen |
| (Beijing Research Institute of Precise Mechatronics and Controls) |
| Abstract: |
| A multidisciplinary integrated design andoptimization method of modular aerospace electromechanical servo system is developed, aiming at solving the difficulty to further improve the performance of the current electromechanical servo system due to the incomplete consideration of coupling factors of design parameters.Firstly, the aerospace electromechanical servo system is modularized from product layer, component layer and part layer. Secondly, the modularized design flow and V-cycle data transmission route are given.Finally, the efficiency of the proposed modular integrated design and optimization method are verified by an engineering example,which practically improves the overall design ability of the aerospace servo system. |
| Key words: Aerospace servo system Multidisciplinary integrated design Modular design |