弹载卫星导航天线结构设计研究
Structure Design of Missile-borne Satellite Navigation Antenna
郑晓东 1王欣伟2
作者信息
- 1. 中国电子科技集团公司第二十研究所,陕西西安 710068
- 2. 西安邮电大学,陕西西安 710121
- 折叠
摘要
在现代战争中,弹载设备是一种重要的攻击和防御手段,其结构设计的可靠性和环境适应性直接影响整机的使用寿命与性能指标.文中介绍了某弹载卫星导航天线的结构设计过程,在给定的结构物理参数条件下,通过理论分析与经验设计,结合有限元仿真手段,提高产品结构设计的质量,以达到各项环境适应性指标要求,保证整机性能指标可靠实现.
Abstract
In the modern warfare,the missile-borne equipment is an important means of attack and defense.The reliability and environmental adaptability of equipment structure design directly affect the service life and performance indicators of the whole equipment.The structure design process of a missile-borne satellite navigation antenna is introduced in this paper.Under the given structural physical parameters,the structure design quality of product is improved through theoretical analysis,empirical design and finite element simulation,so as to meet various environmental adaptability requirements and ensure the reliable realization of the overall performance indicators.
关键词
弹载设备/环境适应性/卫星导航天线/有限元仿真Key words
missile-borne equipment/environmental adaptability/satellite navigation antenna/finite element simulation引用本文复制引用
出版年
2024
NETL
NSTL
万方数据