Literature DB >> 33005110

Monitoring orbital precession of EO-1 Hyperion with three atmospheric correction models in the Libya-4 PICS.

Christopher Neigh1, Joel McCorkel1, Petya Campbell1,2, Laurence Ong1,3, Vuong Ly4, David Landis1,5, Stuart Fry1,6, Elizabeth Middleton1.   

Abstract

Spaceborne spectrometers require spectral-temporal stability characterization to aid validation of derived data products. EO-1 began orbital precession in 2011 after exhausting onboard fuel resources. In the Libya-4 Pseudo Invariant Calibration Site (PICS) this resulted in a progressive shift from a mean local equatorial crossing time of ~10:00 AM in 2011 to ~8:30 AM in late 2015. Here, we studied precession impacts to Hyperion surface reflectance products using three atmospheric correction approaches from 2004 to 2015. Combined difference estimates of surface reflectance were < 5% in the visible near infrared (VNIR) and < 10% for most of the shortwave infrared (SWIR). Combined coefficient of variation (CV) estimates in the VNIR ranged from 0.025 - 0.095, and in the SWIR ranged from 0.025 - 0.06, excluding bands near atmospheric absorption features. Reflectances produced with different atmospheric models were correlated (R 2) in VNIR from 0.25 - 0.94 and SWIR from 0.12 - 0.88 (p < 0.01). The uncertainties in all models increased with terrain slope up to 15° and selecting dune flats could reduce errors. We conclude that these data remain a useful resource over this period.

Keywords:  ACORN; ATREM; EO-1 Hyperion; FLAASH; Libya-4; land surface imaging (LSI); orbital precession; pseudo-invariant calibration site (PICS); surface reflectance; time-series analysis

Year:  2016        PMID: 33005110      PMCID: PMC7526679          DOI: 10.1109/lgrs.2016.2612539

Source DB:  PubMed          Journal:  IEEE Geosci Remote Sens Lett        ISSN: 1545-598X            Impact factor:   3.966


  1 in total

1.  Sand dune ridge alignment effects on surface BRF over the Libya-4 CEOS calibration site.

Authors:  Yves M Govaerts
Journal:  Sensors (Basel)       Date:  2015-02-03       Impact factor: 3.576

  1 in total

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