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Multimodal hybrid powerplant for unmanned aerial systemsud(UAS) robotics

机译:用于无人机系统的多模式混合动力装置 ud(UAS)机器人技术

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摘要

Most UAS propulsion systems currently utilize either Internal Combustion Engines (ICE) or Electric Motorud(EM) prime movers. ICE are favoured for aircraft use due to the superior energy density of fuel compared toudbatteries required for EM, however EM have several significant advantages. A major advantage of EM is thatudthey are inherently self starting have predictable response characteristics and well developed electronic controludsystems. EMs are thus very easy to adapt to automatic control, whereas ICE have more complex controludresponse and an auxiliary starting motor is required for automated starting.udThis paper presents a technique for determining the performance, feasibility and effectiveness of powerplantudhybridisation for small UAS. A Hybrid Powerplant offers the possibility of a radical improvement in theudautonomy of the aircraft for various tasks without sacrificing payload range or endurance capability. In thisudwork a prototype Aircraft Hybrid Powerplant (AHP) was designed, constructed and tested. It is shown that anudadditional 35% continuous thrust power can be supplied from the hybrid system with an overall weight penaltyudof 5%, for a given UAS.udDynamometer and windtunnel results were obtained to validate theoretical propulsion load curves. Usingudmeasured powerplant data and an assumed baseline airframe performance characteristic, theoretical enduranceudcomparisons between hybrid and non-hybrid powerplants were determined. A flight dynamic model for theudAHP was developed and validated for the purposes of operational scenario analysis. Through this simulation itudis shown that climb rates can be improved by 56% and endurance increased by 13%.udThe advantages of implementing a hybrid powerplant have been baselined in terms of payload range andudendurance. Having satisfied these parameters, a whole new set of operational possibilities arises which cannotudbe performed by non-self-starting ICE only powered aircraft. A variety of autonomous robotic aircraft tasksudenabled by the hybrid powerplant is discussed.
机译:当前,大多数UAS推进系统都使用内燃机(ICE)或电动机 ud(EM)原动机。与EM所需的 udbattery相比,ICE具有更高的燃料能量密度,因此ICE在飞机上得到了广泛使用,但是EM具有许多重要的优势。 EM的主要优点是,它们固有的自启动功能具有可预测的响应特性,并且电子控制系统发达。因此,EM非常容易适应自动控制,而ICE具有更复杂的控制响应,并且需要使用辅助启动马达来进行自动启动。 ud本文介绍了一种确定小型动力装置/加氢技术的性能,可行性和有效性的技术。无人机系统。混合动力装置可以在不牺牲有效载荷范围或耐久力的情况下,从根本上改善飞机的各种功能。在这项工作中,设计,制造和测试了飞机混合动力装置(AHP)的原型。结果表明,对于给定的UAS,混合动力系统可以提供常规的35%连续推力,总重量损失 udof5%。 ud测功机和风洞测试结果验证了理论推进载荷曲线。使用测得的动力装置数据和假定的基准机身性能特征,确定了混合动力和非混合动力装置之间的理论耐久性比较。为了进行运行情景分析,开发并验证了 udAHP的飞行动力学模型。通过此模拟,它显示爬升率可以提高56%,而耐力​​则可以提高13%。 ud采用混合动力装置的优势已经在有效载荷范围和耐力方面得到了基线。满足了这些参数后,出现了一套全新的操作可能性,这是非自启动ICE动力飞机无法实现的。讨论了由混合动力装置实现的各种自主机器人飞行器任务。

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