星载大口径环形天线的系统设计OA北大核心
System design of spaceborne large aperture perimeter truss antenna
环形可展开天线是星载大口径、超大口径可展开天线的理想结构形式,是高轨遥感、高轨通信卫星应用的关键载荷.星载环形天线是由周边展开桁架和索网系统组成的典型预应力结构,型面精度和展开基频是其主要性能指标.在轨可靠展开是在轨应用的前提,可靠展开是设计的重中之重,以在轨性能指标需求为目标,分析了环形天线各系统参数对在轨性能指标的影响.通过对展开动力系统和传动力系统进行分析,阐述了环形天线各系统参数对展开可靠性的影响,总结了以结构静力学手段评价在轨性能设计和动力学手段评价展开可靠性的方法,明确了通过结构动力学方法进行强度校核和星上锁紧释放设计的星载大口径环形天线系统设计流程,提出了各设计参数的优化策略,并给出了系统设计算例,为未来超大口径星载可展开天线的技术研究和工程研制提供参考.
The perimeter truss antenna is the ideal structure of the spaceborne deployable antenna with very large aperture,which is the key payload for high-orbit communication and high-orbit remote sensing satellite applications.The spaceborne perimeter truss antenna is a typical prestressed structure composed of the surrounding truss and cable network system.The accuracy of surface and the fundamental frequency of antenna are the main performance indexes of antennas.On-orbit reliable deployment is the premise of on-orbit application,and reliable deployment is the most important part of antenna design.The influence of ring antenna system parameters on on-orbit performance is analyzed.Based on the analysis of the deployable power system and the transmission power system,the influence of system parameters of the ring antenna on the deployable reliability is expounded.The method of evaluating the on-orbit performance design by structural statics and the deployable reliability by dynamic means are proposed.The design flow of spaceborne large aperture perimeter truss antenna system is defined by strength verification and on-board lock-release design by structural dynamics method,and the optimization strategy of each design parameter is proposed.It provides a reference for technical research and engineering development of the larger aperture spaceborne deployable antenna in the future.
冯涛;张庆君;林坤阳;王立朋;张桥;杨军刚;肖勇
西安空间无线电技术研究所,西安 710100中国空间技术研究院 遥感卫星总体部,北京 100094西安空间无线电技术研究所,西安 710100西安空间无线电技术研究所,西安 710100西安空间无线电技术研究所,西安 710100西安空间无线电技术研究所,西安 710100西安空间无线电技术研究所,西安 710100
星载环形天线在轨性能可展开结构系统设计参数优化策略
spaceborne perimeter truss antennaon-orbit performancedeployable structuresystem designoptimization strategy
《中国空间科学技术(中英文)》 2025 (1)
24-33,10
国家自然科学基金(U23B2095)
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