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High Payload UAV System for Civilian Surveillance

机译：高有效载荷无人机系统，用于平民监视

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摘要

A 3.6 m wing span full glass fiber fixed wing UAV isrndesigned and fabricated for high payload surveillancernapplications. To fulfill the critical flight requirements,rna 157 cc engine provides ample power for easyrnmaneuvering. An autopilot flight control systemrncontaining MEMS and microprocessor hardware isrndeveloped for remote operation via multiplerncommunication links. The GPS autopilot follows thernpath plan with navigation waypoints and 3Drnconstraints. For accurate terrain avoidance, real-timernQNH altitude correction is added to GIS flightrnoperation. For image acquisition, high quality camerarnsets are equipped for fast 30 time zoom-in within 1rnsecond. The proposed Cardinal UAV system is testedrnon an ultra-light airfield. Some advanced flightrnperformance data are verified by continuing flightrntest programs including water landing. An additionalrnslotted Krueger flap will modify the UAV for lowrnspeed performance to enhance photo quality. Thernproposed UAV focuses on civilian applications forrnhomeland security, disaster surveillance, rescuernsearch and environment protection.
机译：设计并制造了3.6 m翼展全玻璃纤维固定翼无人机，用于高载荷监视应用。为了满足关键的飞行要求，rna 157 cc发动机提供了充足的动力，易于操纵。开发了一种包含MEMS和微处理器硬件的自动驾驶飞行控制系统，可通过多个通信链路进行远程操作。 GPS自动驾驶仪遵循带有导航航点和3Drn约束的路径规划。为了避开地形，将实时QNH高度校正添加到GIS飞行操作中。为了获取图像，配备了高质量的相机组，可在1秒钟内快速进行30倍放大。拟议的枢机无人机系统是在超轻型飞机场上进行测试的。一些先进的飞行性能数据已通过包括水着陆在内的持续飞行测试程序进行了验证。额外开槽的Krueger襟翼将修改无人机的低速性能，以提高照片质量。拟议的无人机主要用于民用领域，如国土安全，灾难监视，救援研究和环境保护。

著录项

  • 来源
    《Unmanned Air Vehicle Systems(UAVs)》|2010年|p.24.1-24.11|共11页
  • 会议地点 Bristol(GB);Bristol(GB);Bristol(GB)
  • 作者

    Chin E. Lin; Y. H. Lai; Y. C. Huang; C. C. Li; C. J. Sun; C. W. Tu; W. C. Huang; C. C. Nien; C. C. Cheng; M. Y. Shih;

  • 作者单位

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701 chinelin@mail.ncku.edu.tw Tel/Fax: 886-6-2741820/886-6-2361835;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    Department of Aeronautics and Astronautics, National Cheng Kung University Tainan, Taiwan 701;

    ISTC Industrial Technology Research Institute Chu-Tong, Hsin-Chu, Taiwan 310;

    /EOL Industrial Technology Research Institute Chu-Tong, Hsin-Chu, Taiwan 310;

    /ICL Industrial Technology Research Institute Chu-Tong, Hsin-Chu, Taiwan 310;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 无人驾驶飞机;
  • 关键词

    MEMS Avionics; Path Plan Autopilot; QNH Altitude Correction; Surveillance Application;

    机译：MEMS航空电子;路径计划自动驾驶仪； QNH海拔校正；监控应用;

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