临近空间长航时无人机平台天线一体化结构设计

    Structure Design of Platform-antenna Integration for Near Space Long-endurance Unmanned Air Vehicle

    • 摘要: 因具备高空、长航时的独特优势,用于雷达探测的临近空间长航时无人机在空间攻防和信息对抗领域拥有广阔的发展前景。由于临近空间无人机载荷能力限制,雷达探测系统结构及重量需满足飞机平台极其苛刻的要求。平台天线一体化是解决该问题的关键技术之一,通过将天线与飞机平台结构一体化设计,实现天线既是雷达载荷功能件,同时也是飞机平台结构的主或次承力构件。文中将雷达系统中天线与平台结构融合,研究了平台天线一体化结构设计,实现了雷达天线结构功能与平台结构承载功能一体化,阐述了平台天线一体化结构,仿真分析了一体化结构刚度、强度,开展了积木化试验中盒段级结构试验验证。验证结果表明,文中提出的平台天线一体化结构满足装机刚度、强度及稳定性要求。

       

      Abstract: For unique advantages of high altitude long endurance, near space long-endurance unmanned air vehicle using for radar detection possess wide development prospects in areas of space countermeasure and information confrontation. However, the limitation of load capacity leads to extremely harsh requirements on structure and weight of radar detection system. Platform-antenna integration is one of the key techniques to deal with this problem. Through the integrated design of antenna and air vehicle structure, antenna structure is the functional part of radar system, and also be the primary or secondary load-bearing part of air vehicle. In this paper, the antenna of radar system is integrated with platform structure; the platform-antenna integrated structure design is studied, and the integration of radar antenna structure function and the platform structure bearing function is achieved. The platform-antenna integrated structure is elaborated, and the simulational analysis of the stiffness and strength of integrated structure is carried out. The box-level structure verification testing by means of building block approach (BBA) is conducted. The results of structural strength test illustrate that the proposed platform-antenna integrated structure satisfies the requirements of stiffness, strength and stability.

       

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