航空学报 > 2023, Vol. 44 Issue (6): 27034-027034   doi: 10.7527/S1000-6893.2022.27034

传感器飞机核心关键技术进展与应用

郝帅1,2, 马铁林3, 王一1, 向锦武1(), 马洪忠2, 蒋柏峰4, 曹军5   

  1. 1.北京航空航天大学 航空科学与工程学院,北京 100083
    2.海鹰航空通用装备有限责任公司,北京 100074
    3.北京航空航天大学 无人系统研究院,北京 100083
    4.中国电子科学研究院,北京 100041
    5.南京电子设备研究所,南京 211103
  • 收稿日期:2022-02-14 修回日期:2022-03-03 接受日期:2022-03-14 出版日期:2023-03-25 发布日期:2022-03-22
  • 通讯作者: 向锦武 E-mail:xiangjw@buaa.edu.cn
  • 基金资助:
    国家自然科学基金(91216102)

Progress and application of key technologies of SensorCraft

Shuai HAO1,2, Tielin MA3, Yi WANG1, Jinwu XIANG1(), Hongzhong MA2, Baifeng JIANG4, Jun CAO5   

  1. 1.School of Aeronautic Science and Engineering,Beihang University,Beijing 100083,China
    2.Hiwing General Aviation Equipment Co. ,Ltd. ,Beijing 100074,China
    3.Research Institute of Unmanned Systems,Beihang University,Beijing 100083,China
    4.China Academy of Electronics and Information Technology,Beijing 100041,China
    5.Nanjing Electronic Equipment Institute,Nanjing 211103,China
  • Received:2022-02-14 Revised:2022-03-03 Accepted:2022-03-14 Online:2023-03-25 Published:2022-03-22
  • Contact: Jinwu XIANG E-mail:xiangjw@buaa.edu.cn
  • Supported by:
    National Natural Science Foundation of China(91216102)

摘要:

传感器飞机是美国空军实验室提出的一种高空长航时预警监视和信息综合飞行器,采用平台载荷一体化技术理念,兼具飞行器和传感器的双重特征。平台与载荷之间多要素耦合,意味着不同于传统情报、监视与侦察(ISR)飞机的总体设计;飞行条件与性能指标为气动设计带来了新挑战;大展弦比柔性机翼的气动弹性问题不仅造成飞行性能恶化,还会导致机翼共形天线电性能的损失。本文总结了传感器飞机的技术特征,从飞行平台和共形天线两方面阐述了美国传感器飞机系统的发展历程,梳理了支撑传感器飞机发展的一体化布局设计、层流减阻、阵风减缓、共形天线设计、形变测量与重构、电性能补偿6项核心关键技术并介绍了相关应用;从飞行能力、隐身能力、感知能力及协同能力4个方面展望了该类飞行器的发展趋势,可为后续新型ISR飞机提供参考。

关键词: 传感器飞机, 一体化设计, 飞行平台, 共形天线, 预警监视

Abstract:

SensorCraft is an early warning and surveillance and information synthesis aircraft proposed by the Air Force Research Laboratory, with high ceiling and long endurance. It adopts the platform-payload integration technology, with the dual features of the aircraft and sensor. Coupling of multiple elements between platform and payload means that the overall layout design is different from that of the traditional Intelligence, Surveillance and Reconnaissance (ISR) vehicle. Flight conditions and performance indexes bring new challenges to the aerodynamic design. Aeroelastic problem of large aspect ratio flexible wing not only worsens flight performance, but also leads to loss of electromagnetic performance of wing conformal antenna. This paper summarizes the technical characteristics of SensorCraft, expounds the development history of the United States SensorCraft system from two aspects of the flight platform and conformal antenna. From the perspective of technical characteristics, key technologies supporting SensorCraft are sorted out, such as integrated layout design, laminar drag reduction, gust alleviation, conformal antenna design, deformation measurement & reconstruction, and electromagnetic performance compensation. Relevant applications are introduced. The development trend of this aircraft is also discussed in terms of the flight ability, stealth ability, perception ability and coordination ability of the aircraft, so as to provide reference for the new ISR aircraft.

Key words: SensorCraft, integrated design, flight platform, conformal antenna, early warning and surveillance

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