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CASCADE Open Aircraft Project: University of Southampton VTOL Drone Development

机译:级联开放式飞机项目:南安普敦大学VTOL无人驾驶

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The Open Aircraft Project is an initiative by the UK Complex Autonomous Aircraft Systems Configuration, Analysis, and Design Exploratory (CASCADE) Programme Grant team to create small unoccupied aerial system (SUAS) designs which are freely available to all. Starting with a representative but challenging set of mission requirements, two individual teams have designed, built and test flown competing vertical take-off and landing (VTOL) configurations. This paper describes the contribution made to this project by the University of Southampton with an investigation into the design, manufacture and testing of an unoccupied aerial vehicle (UAV) capable of transitioning from hovering flight to conventional fixed-wing forward flight with vertical take-off and landing. Two configurations were investigated with the aim of achieving precision in take-off and landings with a comparably efficient long-range flight. The ability to perform vertical take-off and landing removes the requirement for a prepared airstrip with an unobstructed approach, which is often a serious constraint in the operation of conventional fixed-wing aircraft. This paper first explored the merits of a tail-sitter aircraft, with an emphasis on the minimisation of both the number of required propulsion sources and actuation devices for conducting relatively long-range investigative scientific missions. Flight testing of the tail-sitter aircraft revealed a number of unfavourable flight dynamics, which ultimately led to the decision to divert the investigation to the performance of a quad-plane configuration with the same requirements. The quad-plane design proved to be robust and able to operate effectively with an increased wind tolerance when compared to the tail-sitter design. Initial calculations based on a series of test flights suggest the quad-plane design, whilst carrying a reduced payload, will be capable of fulfilling the endurance and altitude requirements of the mission successfully.
机译:开放式飞机项目是英国复杂的自主飞机系统配置,分析和设计探索(Cascade)计划补助团队的主动权,以创建小型无人居的空中系统(SUAS)设计,这些设计是自由的。从代表性但具有挑战性的任务要求开始,两个单独的团队已经设计,建造和测试竞争垂直起飞和着陆(VTOL)配置。本文介绍了南安普顿大学对该项目的贡献,并调查了能够从悬停飞行到传统的固定翼前向前飞行的无人居住的空中车辆(UAV)的设计,制造和测试进行了调查和着陆。调查了两种配置,目的是实现在起飞和着陆方面的精确度,具有相对有效的远程飞行。执行垂直起飞和着陆的能力消除了具有无阻碍方法的制备的空气仪的要求,这通常是传统固定翼飞机的操作中的严重限制。本文首先探讨了尾部保姆飞机的优点,重点是最小化所需推进源和致动装置的最小化,用于进行相对远程调查科学任务。尾部保姆飞机的飞行测试揭示了许多不利的飞行动态,最终导致决定将调查转移到具有相同要求的四面板配置的性能。与尾部设施设计相比,四方平面设计被证明是坚固的并且能够有效地通过增加的风耐耐力操作。基于一系列测试航班的初始计算表明了四面机设计,同时携带减少的有效载荷,将能够成功实现任务的耐用性和高度要求。

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