According to the design method of the high-altitude ultra-long-endurance high-aspect-ratio integrated unmanned aerial vehicle platform, full-platform design of a rectification antenna is considered from the perspective of overall integration, transmissibility and relevance of parameters such as overall parameters, pneumatic parameters and structural parameters are fully considered, and a detailed design stage is started; in other words, the sub-component design under the constraint of the integrated platform can be adopted to accelerate the iteration process. According to the method, constraint conditions and design indexes are decomposed through an integrated thought, interactive design is carried out on the platform and the antenna, finally modular research and development under integration are achieved, the rectification antenna is combined with the platform in an integrated module mode, and the antenna and the platform can integrally form a whole system through a simple connection relation.
本发明提出一种高空超长航时大展弦比一体化无人飞行平台设计方法,从整体一体化的角度进行考虑整流天线的全平台设计,充分考虑各个总体、气动、结构等参数的传递性和关联性,而进入详细设计阶段,即可以采用一体化平台约束下的分部件设计以加快迭代流程。本发明中,通过一体化的思路分解约束条件和设计指标,在平台和天线上进行交互设计,最终实现了一体化下的模块化研发,整流天线以一体化模块的形式与平台结合,也即通过简单的连接关系即可将天线与平台完整的组成一个整体系统。
Design method of high-altitude ultra-long-endurance high-aspect-ratio integrated unmanned flying platform
一种高空超长航时大展弦比一体化无人飞行平台设计方法
2022-11-29
Patent
Elektronische Ressource
Chinesisch
IPC: | G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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