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Design and Test of a Sonobuoy Precision Aerial Delivery (SPAD) UAV System

机译:Sonobuoy精密空中交付(SPAD)UAV系统的设计与测试

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A Sonobuoy Precision Aerial Delivery (SPAD) UAV glider system that enables GPS-controlled placement of antisubmarine warfare acoustic sensors has been developed. Unlike the current placement method, which deploys the sonobuoy via uncontrolled parachute decent, the unpowered SPAD provides 27 mile stand-off range and precise GPS-guided sensor placement to enhance signal processing accuracy. SPAD is designed to conform to existing launch tube geometry which enables use of legacy sensors (sonobuoys) and infrastructure (launchers and launch aircraft). This constraint has significant influence on the air vehicle design. SPAD's flight path is programmed aboard the launch aircraft and SPAD is then tube-launched over a wide range of speeds and altitudes up to 30,000 feet. Wings and unique grid fin control surfaces deploy after launch and the vehicle flies a prescribed flight plan down to a low altitude, whereupon the sonobuoy payload ejects from the SPAD. The sonobuoy enters the water after a brief parachute decent to deploy hydrophones up to a 1000' depth. The launch tube form factor constraints, high payload mass, Cartridge Actuated Device (CAD) explosive launch from a high speed aircraft, deployable wings, and compact grid fins control surfaces were challenging design features. Significant wind tunnel testing was conducted and is described. Alternative payloads are also currently under development and are summarized.
机译:已经开发出一种Sonobuoy精密空中传送(SPAD)UAV滑翔机系统,其能够进行GPS控制的防野战争判声学传感器。与通过不受控制的降落伞体面部署Sonobuoy的当前放置方法不同,无动力的SPAD提供27英里的脱扣范围和精确的GPS引导传感器放置,以提高信号处理精度。 SPAD旨在符合现有的发射管几何形状,可以使用传统传感器(Sonobuoys)和基础设施(发射器和发射机)。该约束对空气车辆设计产生了重大影响。 Spad的飞行路径被编程,推出飞机并将其剥片在一起,速度范围内,高达30,000英尺的速度。发射后翅膀和唯一的网格鳍控制表面部署,车辆将规定的飞行计划降至低空,从而从Sonobuoy有效载荷从Spad弹出。在短暂的降落伞体面展开高度为1000'深度后,Sonobuoy进入水。发射管形式因子约束,高有效载荷质量,墨盒驱动装置(CAD)爆炸发射从高速飞机,可展开的翅膀和紧凑型网格翅片控制表面挑战设计特征。进行了显着的风洞测试并描述。替代有效载荷目前正在开发中,总结。

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