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UAVSAR: A new NASA airborne SAR system for science and technology research

机译:UAVSAR:用于科学和技术研究的新型NASA机载SAR系统

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摘要

NASA’s Jet Propulsion Laboratory is currentlyudbuilding a reconfigurable, polarimetric L-band syntheticudaperture radar (SAR), specifically designed to acquire airborneudrepeat track SAR data for differential interferometricudmeasurements. Differential interferometry can provide keyuddeformation measurements, important for studies ofudearthquakes, volcanoes and other dynamically changingudphenomena. Using precision real-time GPS and a sensorudcontrolled flight management system, the system will be able toudfly predefined paths with great precision. The expectedudperformance of the flight control system will constrain the flightudpath to be within a 10 m diameter tube about the desired flightudtrack. The radar will be designed to be operable on a UAVud(Unpiloted Arial Vehicle) but will initially be demonstrated on audon a NASA Gulfstream III. The radar will be fully polarimetric,udwith a range bandwidth of 80 MHz (2 m range resolution), andudwill support a 16 km range swath. The antenna will beudelectronically steered along track to assure that the antennaudbeam can be directed independently, regardless of the winduddirection and speed. Other features supported by the antennaudinclude elevation monopulse and pulse-to-pulse re-steeringudcapabilities that will enable some novel modes of operation. Theudsystem will nominally operate at 45,000 ft (13800 m). Theudprogram began as an Instrument Incubator Project (IIP) fundedudby NASA Earth Science and Technology Office (ESTO).
机译:美国国家航空航天局的喷气推进实验室目前正在 u建造一个可重新配置的极化L波段合成孔径雷达(SAR),该雷达专门设计用于获取机载重复轨道SAR数据,以进行差分干涉测量/测距。差分干涉测量法可以提供关键的变形测量,这对于研究地震,火山和其他动态变化 udphenomena非常重要。使用精确的实时GPS和传感器受udud控制的飞行管理系统,该系统将能够 undud非常精确的预定义路径。飞行控制系统的预期 ud性能将约束飞行 udpath在围绕所需飞行 udtrack的直径10 m的管内。该雷达将设计为可在无人飞行器(UAV)上运行,但最初将在NASA湾流III上进行演示。雷达将是全极化的,具有80 MHz的范围带宽(2 m范围分辨率),并且将支持16 km的范围。天线将沿轨道电子导航,以确保无论风向和速度如何,天线都可以独立定向。天线 ud支持的其他功能包括仰角单脉冲和脉冲到脉冲的重新控制能力,这将使某些新颖的操作模式成为可能。该系统将在45,000英尺(13800 m)处正常运行。该 ud方案最初是由美国国家航空航天局地球科学技术办公室(ESTO)资助 ud的一个仪器孵化器项目(IIP)。

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