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Design, development and operation of uavs for remote sensing

机译:无人机的设计,开发和运行

摘要

The Flight Research Lab, in partnership with the Center for Remote Sensing of Ice Sheets (CReSIS), has developed an ice-penetrating radar system on a 1100 lb gross takeoff weight/100 lb payload UAV. Based on radar miniaturization, a UAV with a 75 lb gross takeoff weight/20 lb payload has recently been designed and is currently in flight test. Both systems were designed based on the radar system requirements. For the 1100 lb Meridian, the radar mass and flight range dictated the size of the aircraft, and resulted in a unique spot in design space not available from existing vehicles. For the 75 lb YAK/G1X, an available “kit” aircraft nearly fit the bill, but a larger wing was needed for the radar; so a longer wing was designed for the stock fuselage. CReSIS and KU Composites Lab teams have fielded numerous radar systems for crewed aircraft including the DC-8, P-3 and Twin Otter. These radar have imaged bedrock beneath as much as 3.5 km of ice in Antarctica, giving glaciologists never-before seen glimpses of the topography of the continent. Now, radar have been designed for UAVs with the goal of reducing the danger of human flight over glaciers. [Last year a Twin Otter crew was lost in Antarctica in a quickly-moving storm.] The Flight Research Lab has developed a design/build/test process to provide semi-autonomous, remote sensing UAV platforms to meet unique sensing needs. Full-time staff is augmented by talented undergrads and graduate students who work on the team as they learn relevant analysis, design, fabrication and test skills. Flight test partners include private contractors, Kansas businesses and the KSU Aviation Technology Department. Some of the unique design features to be discussed include:• Carbon fiber and glass fiber structures augmented with both aluminum and wood substructure• Customized avionics (autopilot, navigation, communications and power distribution)• Quasi-real-time simulation processes for nonlinear aircraft dynamics identification and control system design, which enable smaller UAVs which are more agile (think able to avoid others)Some of the evolving technologies to be discussed include “flight director” systems coupling autopilot, navigation and situational awareness systems for see/sense & avoid capability, including cognitive architectures for on-board decision-making.
机译:飞行研究实验室与冰原遥感中心(CReSIS)合作开发了一种在1100 lb总起飞重量/ 100 lb有效载荷无人机上的穿透冰的雷达系统。基于雷达的小型化,最近已经设计出总起飞重量为75磅/有效载荷为20磅的无人机,目前正在飞行测试中。两种系统都是根据雷达系统要求设计的。对于1100磅的子午线,雷达的质量和飞行范围决定了飞机的大小,并在设计空间中形成了一个独特的点,而现有车辆无法提供这一点。对于75磅的YAK / G1X,可用的“成套”飞机几乎可以满足要求,但是雷达需要更大的机翼。因此为机体机身设计了更长的机翼。 CReSIS和KU Composites Lab团队已经为无人驾驶飞机部署了许多雷达系统,包括DC-8,P-3和Twin Otter。这些雷达成像了南极长达3.5公里的冰下的基岩,为冰川学家提供了前所未有的大陆地形概况。现在,已经为无人飞行器设计了雷达,目的是减少人类越过冰川飞行的危险。 [去年,在快速变化的风暴中,双水獭机组人员在南极失踪。]飞行研究实验室已经开发出一种设计/建造/测试过程,以提供半自主的,遥感UAV平台,以满足独特的传感需求。全职员工充实了优秀的本科生和研究生,他们在团队中学习相关的分析,设计,制造和测试技能。飞行测试的合作伙伴包括私人承包商,堪萨斯州的企业和KSU航空技术部门。有待讨论的一些独特设计特征包括:•铝和木质子结构增强的碳纤维和玻璃纤维结构•定制的航空电子设备(自动驾驶仪,导航,通信和功率分配)•非线性飞机动力学的准实时仿真过程识别和控制系统设计,使较小的无人机更敏捷(认为能够避免其他攻击)讨论中的一些不断发展的技术包括结合自动驾驶,导航和态势感知系统的“飞行指挥”系统,以查看/感知并避免能力,包括用于机上决策的认知架构。

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    Ewing Mark S.;

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  • 年度 2013
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