随着近年来无人机技术的迅猛发展，世界多国开始将更多的资金投入到大尺寸喷气式察打一体舰载无人机的研发上，并让高速旋转隐身舰载无人机在各个技术领域进行转型升级，力求在未来战争中获得更大的胜利可能。目前，美国、俄罗斯、中国、英国和法国等国可以进行高性能舰载无人机的研究，这些国家的舰载无人机具有共性，如高速性、高空性、隐身性和远程性、高感知能力和高打击能力等，其“四性两高”的特征，使其在未来战争中起到扭转形势的重要作用。本文结合目前的相关参数信息，对舰载无人机的外形展开设计，旨在提升其性能，节约制造成本，为舰载无人机研发提供参考。
With the rapid development of UAV technology in recent years, many countries in the world have begun to invest more funds in the research and development of large-scale jet-type surveillance and strike integrated carrier-based UAVs, and let high-speed rotating stealth carrier-based UAVs in various The technological field has undergone transformation and upgrading, striving to achieve a greater possibility of victory in future wars. At present, among countries in the world, countries such as the United States, Russia, China, the United Kingdom, and France can conduct research on high-performance carrier-based UAVs. The carrier-based UAVs in these countries have common characteristics, such as high speed, High-altitude, stealth and long-range, high perception capability and high strike capability, etc., its “four characteristics and two high” characteristics make it play an important role in reversing the situation in future wars. Based on the current relevant parameter information, this paper tentatively designs the shape of the carrier-based UAV, aiming to improve its performance, save manufacturing costs, and bring some references for development of carrier-based UAVs.
2023,45(14): 94-97 收稿日期：2023-4-10
DOI：10.3404/j.issn.1672-7649.2023.14.017
分类号：U667.65
基金项目：河南省杰出外籍科学家工作室资助项目（GZS2020009）；郑州航院研究生教育改革与发展研究项目（2022YJSJG34）；郑州航院教育教学改革研究与实践项目（zhjysc22-15）
作者简介：焦斌(1978-),男,硕士,副教授,研究方向为产品设计及可穿戴产品设计。
参考文献：
[1] 安金坤, 方峰, 曾巍. 一种基于双测度的参数重叠舰载雷达型号自动识别方法[J]. 电子信息对抗技术, 2022, 37(3): 16–19+25
[2] 崔恒荣, 秦雅, 卞玮章. 基于模糊控制参数自整定的舰载雷达三轴稳定控制[J]. 雷达与对抗, 2020, 40(1): 57–60
[3] 邓恩民, 刘冬利, 侯建强, 等. 基于参数反演的舰载雷达探测威力预报方法[J]. 空军预警学院学报, 2021, 35(3): 188–190+201
[4] 韩维, 崔凯凯, 刘洁, 等. 基于自校正MPC的舰载机着舰控制技术[J]. 系统工程与电子技术, 2022, 44(1): 250–261
[5] 晋文超, 李鹏, 李亚军, 等. 舰载机起降限制区域及主要影响参数[J]. 中国舰船研究, 2016, 11(5): 28–34
[6] 朱齐丹, 王立鹏, 张智, 等. 舰载机着舰侧回路时变风险权值矩阵线性变参数预测控制[J]. 控制理论与应用, 2015, 32(1): 101–109
