Characterization of MODIS SD screen vignetting function using observations from spacecraft yaw maneuvers

Zhipeng Wang; Xiaoxiong Xiong

doi:10.1117/12.824656

21 August 2009 Characterization of MODIS SD screen vignetting function using observations from spacecraft yaw maneuvers

Zhipeng Wang, Xiaoxiong Xiong

Proceedings Volume 7452, Earth Observing Systems XIV; 745217 (2009) https://doi.org/10.1117/12.824656
Event: SPIE Optical Engineering + Applications, 2009, San Diego, California, United States

Abstract

The MODIS reflective solar bands (RSB) include both the low-gain and high-gain spectral bands depending on their specific applications. MODIS RSBs are calibrated on-orbit by an on-board solar diffuser. In order to avoid detector response saturation when calibrating the high-gain bands, an optional attenuation screen, made of a metal plate with pinhole arrays, is placed in front of the SD panel. Since no pre-launch system-level characterization was made for the SD screen (SDS) vignetting function (VF), a series of spacecraft (Terra and Aqua) yaw maneuvers were carried out to perform on-orbit characterization of the VF. Assuming that the low-gain bands and the high-gain bands have the same VF, the current VF was derived from yaw observations using the MODIS low-gain bands through taking the ratio of their SD responses with and without the SDS in place. In this study, we attempt to characterize the SDS VF directly using detector responses of individual high-gain bands with the SDS in place only. The corresponding SD responses without the SDS, not available from measurements due to saturation, are calculated using detector gains, the SD bi-directional reflectance factor (BRF), and the view geometry that matches the yaw observations with the SDS in place. Results and discussions are focused on the band dependent and detector dependent features of the SDS VF, and their potential impact on the RSB calibration.

Citation Download Citation

Zhipeng Wang and Xiaoxiong Xiong "Characterization of MODIS SD screen vignetting function using observations from spacecraft yaw maneuvers", Proc. SPIE 7452, Earth Observing Systems XIV, 745217 (21 August 2009); https://doi.org/10.1117/12.824656

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