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MEDUSA, an ultra light weight multi-spectral camera for a HALE UAV

机译:MEDUSA,用于HALE无人机的超轻量多光谱摄像机

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The ESA-PRODEX funded MEDUSA project aims to develop a light weight high resolution multi-spectral earth observation instrument, which will be embarked on a solar-powered high altitude long endurance (HALE) UAV, operated at stratospheric altitudes (15 to 18km). The MEDUSA instrument is designed to fill the gap between traditional airborne and spaceborne instruments regarding resolution and coverage. It targets applications such as crisis management and cartography, requiring high resolution images with regional coverage, flexible flight patterns, high update rates and long mission lengths (weeks to months). The MEDUSA camera is designed to operate at a ground resolution of 30 cm at 18 km altitude in the visible spectrum (400-650 nm), and a swath of 3000m. The central part of the payload is a focal plane assembly consisting of two frame sensors (PAN and RGB). The wide swath is realized with a custom designed highly sensitive CMOS sensor of 10000×1200 pixels. A GPS receiver and Inertial Measurement Unit (IMU) provide accurate position and attitude information. A direct downlink allows near-real time data delivery to the user. The on-board data processing consists mainly of basic image corrections and data compression (JPEG2000). The challenge lies mainly in fulfilling the requirements within the extreme environmental and physical constraints of the HALE UAV. Compared to traditional airborne and spaceborne systems, the MEDUSA camera system is ultra light weight (about 2 kg) and is operated in a low pressure and low temperature environment. System modeling and simulation is used to make careful trade-offs between requirements and subsystem performances.On 27th November 2006 the phase C/D for the design, production and test of the camera has started at VITO with the support of 9 industrial partners. The MEDUSA camera is expected to transmit its first images the end of 2008.
机译:由ESA-PRODEX资助的MEDUSA项目旨在开发一种轻型高分辨率多光谱地球观测仪器,该仪器将搭载在平流层高度(15至18公里)上运行的太阳能高海拔长寿命(HALE)无人机上。 MEDUSA仪器旨在填补传统机载和星载仪器之间在分辨率和覆盖率方面的空白。它的目标是危机管理和制图等应用,需要具有区域覆盖,高分辨率的飞行模式,高更新率和较长任务期限(数周至数月)的高分辨率图像。 MEDUSA摄像机设计为在18 km高度的可见光谱(400-650 nm)中以30 cm的地面分辨率和3000m的范围运行。有效载荷的中心部分是焦平面组件,由两个框架传感器(PAN和RGB)组成。宽幅是通过定制设计的10000×1200像素高灵敏度CMOS传感器实现的。 GPS接收器和惯性测量单元(IMU)提供准确的位置和姿态信息。直接下行链路允许近实时地将数据传送给用户。车载数据处理主要包括基本图像校正和数据压缩(JPEG2000)。挑战主要在于在HALE无人机的极端环境和物理约束下满足要求。与传统的机载和星载系统相比,MEDUSA摄像头系统具有超轻的重量(约2千克),可在低压和低温环境下运行。系统建模和仿真用于在需求和子系统性能之间进行仔细权衡。2006年11月27日,在9个工业合作伙伴的支持下,VITO的相机设计,生产和测试阶段C / D开始。 MEDUSA相机有望在2008年底前传输其第一张图像。

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