Sonotube compatible unmanned aerial vehicle and system
    131.
    发明授权
    Sonotube compatible unmanned aerial vehicle and system 失效
    Sonotube兼容无人机和系统

    公开(公告)号:US6056237A

    公开(公告)日:2000-05-02

    申请号:US882368

    申请日:1997-06-25

    Abstract: The present invention is generally comprised of a sonotube-compatible unmanned aerial vehicle apparatus, hereinafter referred to as a UAV, and systems for launch and control of the UAV. The UAV is generally comprised of modular sections including a nose section, a payload section, a wing and fuel tank section, and a powerplant section. The modular sections are attached to adjacent sections by uniform lock sealing rings and related components. The present invention comprises an apparatus enabling very small, man portable, ballistically launched, autonomously or semi-autonomously controlled vehicle to be deployed with preprogrammed, communicated, or telemetry mission programming. A wide range of payload packages, including emergency supplies, sensors, and antenna assemblies, may be carried, used or deployed in flight. Man-portable operation is accomplished by the use of a launch canister apparatus. The launch canister comprises retractable launch stabilizing legs, turbine engine exhaust orifices, and various antennas. The launch canister apparatus alternatively comprises a modified type "A", "B", or "C" sonotube launch canister. The system of the invention also comprises a portable Command, Control, Communications, Computer, and Intelligence (C4I) control and sensing analysis console. The console is preferably ruggedized, waterproof, shockproof, and comprises necessary control and analysis computers, input/output devices, antennas, and related hardware and software for vehicle and mission control. A C4I console and/or launch canisters may be transported by means of a backpack adapted for man portability.

    Abstract translation: 本发明通常由声纳管相容的无人驾驶飞行器装置(以下称为无人机)和用于发射和控制无人机的系统组成。 无人机通常包括模块化部分,包括鼻部,有效载荷部分,机翼和燃料箱部分以及动力装置部分。 模块化部分通过均匀的锁定密封环和相关部件连接到相邻部分。 本发明包括一种能够进行预编程,通信或遥测任务编程的非常小的,便携式的,弹道发射的,自主的或半自主控制的车辆的装置。 可以在飞行中携带,使用或部署各种有效载荷包,包括应急用品,传感器和天线组件。 便携式操作通过使用发射罐装置来实现。 发射罐包括可伸缩发射稳定腿,涡轮发动机排气孔和各种天线。 发射罐装置可选地包括修改型“A”,“B”或“C”型超声波发射罐。 本发明的系统还包括便携式命令,控制,通信,计算机和智能(C4I)控制和感测分析控制台。 控制台最好是坚固耐用,防水,防震,并且包括必要的控制和分析计算机,输入/输出设备,天线以及用于车辆和任务控制的相关硬件和软件。 C4I控制台和/或发射罐可以通过适于人的便携性的背包来运输。

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