RazakSAT™的飞行前辐射校准

Ng Su Wai, Adhwa Amir Tan, Jessie Mee, M. Ismail, M. Subari
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引用次数: 3

摘要

RazakSAT™是马来西亚的第二颗地球观测卫星。中型孔径相机(MAC)是RazakSAT™上飞行的仪器有效载荷。MAC工作于可见光和近红外波段,包括450nm - 890nm的四个多光谱波段和510nm - 730nm的一个全色波段。多光谱波段地面像素分辨率为5m,全色波段为2.5m。在685公里标称高度,MAC的图像带宽度为20公里。RazakSAT™计划于2009年4月发射到倾角为9°的近赤道轨道(NEqO)。它为与地面站的通信提供了大量的通道(每天在马来西亚上空14次),与太阳同步轨道相比,成像机会增加了3倍。为了给用户提供操作图像的质量保证,进行了地面标定(飞行前标定)。本报告概述了在飞行前校准MAC系统辐射响应时采用的技术。给出并讨论了仪器响应的系统级测量结果,即暗响应、信噪比(SNR)、饱和亮度、动态范围、单个探测器的特性、增益和每个光谱带的线性分析。
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Preflight radiometric calibration of RazakSAT™
RazakSAT™ is Malaysia's second earth observation satellite. The Medium-sized Aperture Camera (MAC) is the instrument payload to be flown on the RazakSAT™. MAC operates on visible and near infrared wavelength (VNIR), including four multispectral bands from 450nm – 890nm and one panchromatic band from 510nm to 730nm. Its ground pixel resolution is 5m for multispectral bands and 2.5m for panchromatic band. At 685km nominal altitude, the image swath width for MAC is 20km. RazakSAT™ is scheduled to be launched into 9° inclination Near-Equatorial Orbit (NEqO) on April 2009. It provides a high number of passes (14 times per day over Malaysia) for communication with ground station, and imaging opportunity increases by 3 times more compared to a sun-synchronous orbit. In order to give user quality assurance of the operational imagery, ground calibration (pre-flight calibration) has been conducted. This report outlines the techniques adopted during pre-flight calibration of the radiometric response of the MAC system. Results from system level measurement of the instrument response, namely the dark response, signal-to-noise ratio (SNR), saturation radiance, dynamic range, characterization of individual detector, gain and linearity analysis for each spectral band are presented and discussed.
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