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Expanding the Mission Capabilities of a Quadrotor Biplane Tail-sitter with Morphing Winglets

机译:借助变形小翼扩展四旋翼双翼飞机尾翼保镖的任务能力

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Multi-mode air vehicles with hover and high cruise speed capabilities can meet a wide range of mission requirements but are limited in their performance in either mode due to the design compromises that come from operating across a wide speed range. This paper describes and evaluates mission-planning strategies for a quadrotor biplane tail-sitter vehicle with a folding winglet system. The winglets offer two configurations that improve aerodynamic efficiency at different airspeeds at the cost of increased airframe mass. Flight data from a prototype vehicle developed at the University of Maryland is used to form an empirical model for power consumption in the two modes. Autonomous flight planning profiles designed to leverage these improvements in aerodynamic performance are implemented in simulation for three representative scenarios. Homogenous teams of morphing-capable vehicles are used in a search and rescue mission, a counter-poaching pursuit-evasion scenario, and in a perimeter defense application. Statistics are gathered from simulated tests with randomly generated objectives to assess mission performance. Current results show that when operated with the same deployment strategies, quadrotor biplane teams enjoy improvements in target acquisition speed and energy consumption over conventional rotorcraft platforms due to their improved aerodynamic efficiency in cruise. Quadrotor biplanes that are able to reconfigure in flight enjoy only modest improvements compared to a fixed box configuration in a search-and-rescue role, and a more significant improvement in a counter-poaching mission. Wing morphing offers more significant advantages in a perimeter defense scenario that requires a wider range of flight speeds; Simulation results show that in this capacity, the morphing elements can offer the operational effectiveness of a high-speed platform along with the improved efficiency enjoyed by a dedicated low-speed wing configuration. In the base defense trials simulated, this translated to a larger defendable perimeter with the same number of vehicles, power savings that allow a bigger team to be fielded for the same power, or the same mission effectiveness of having one less intruder attacking the perimeter.
机译:具有悬停和高巡航速度功能的多模式飞行器可以满足多种任务要求,但由于在宽速度范围内运行而导致的设计折衷,因此在任何一种模式下的性能都受到限制。本文描述并评估了带有折叠小翼系统的四旋翼双翼飞机尾翼保卫车辆的任务计划策略。小翼提供两种配置,以增加机身质量为代价,提高了不同空速下的空气动力学效率。来自马里兰大学开发的原型车的飞行数据被用于形成两种模式下功耗的经验模型。针对三种代表性场景,在仿真中实现了旨在利用空气动力学性能的这些改进而设计的自主飞行计划配置文件。具有变型能力的车辆的均质团队用于搜索和救援任务,反偷猎追击逃避场景以及外围防御应用。从具有随机生成目标的模拟测试中收集统计信息,以评估任务绩效。当前结果表明,以相同的部署策略进行操作时,由于四旋翼双翼飞机团队在巡航中提高了空气动力学效率,因此与传统旋翼飞机平台相比,其目标获取速度和能耗得到了改善。与在搜索和救援角色下的固定箱配置相比,能够在飞行中进行重新配置的四旋翼双翼飞机仅获得了适度的改进,而在反偷猎任务中则有了更大的改进。机翼变形在需要更广泛的飞行速度范围的外围防御场景中提供了更多的显着优势。仿真结果表明,在这种能力下,变形要素不仅可以提供高速平台的运营效率,而且可以通过专用的低速机翼配置提高效率。在模拟的基础防御试验中,这可以用相同数量的车辆转化为更大的可防御范围,以节省功率,从而可以使更大的团队获得相同的能力,或者具有相同的任务效率,即只需较少的入侵者即可攻击该范围。

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