Abstract

The Landsat 8 (L8) spacecraft and its two instruments, the operational land imager (OLI) and thermal infrared sensor (TIRS), have been consistently characterized and calibrated since its launch in February 2013. These performance metrics and calibration updates are determined through the U.S. Geological Survey (USGS) Landsat image assessment system (IAS), which has been performing this function since its launch. The TIRS on-orbit geometric calibration procedures include TIRS-to-OLI alignment, TIRS sensor chip assembly (SCA) alignment, and TIRS band alignment. In December 2014, the TIRS instrument experienced an anomalous condition related to the instrument’s ability to accurately measure the location of the scene select mechanism (SSM). The SSM is a rotating mirror that allows the instrument’s field of view to be pointed at the Earth, for normal imaging, or at either deep space or an onboard black body, for radiometric calibration purposes. This anomalous condition in the SSM’s position sensor made it necessary to implement a new mode of operation for this mirror, termed mode-0. Mode-0 involves operating the mirror in an open-loop control state during normal mission operations when acquiring Earth data. Closed-loop mode-4 is needed for directing the mirror towards the radiometric calibration targets and is used approximately once every two weeks to collect radiometric calibration data. Mode-0 is used for most operational imaging because it does not require SSM encoder data, thereby allowing the SSM encoder electronics to remain unpowered most of the time, reducing its use throughout the lifetime of the TIRS instrument, thus helping to preserve its nominal behavior during it use. This paper discusses the geometric calibration of the SSM mirror during its current normal mode-0 set of image operations, as its open-loop control allows the mirror to drift over time in its uncontrolled state and its effects on products. The results shown in this paper demonstrate that the ability to have ongoing updates to the modeling of the TIRS SSM mirror model, in both an automated fashion and with a set of more manual operations, allows accuracy that approaches mode-4 results within days from the start of a mode-0 event.

Highlights

  • Introduction copyright protection is available forThe Landsat 8 (L8) spacecraft was launched on 11 February, 2013 [1,2,3]

  • Because the Earth collects are imaged in open-loop control, without powering the select mechanism (SSM) motor, specially developed algorithms are used to estimate the position of the SSM mirror from the thermal infrared sensor (TIRS) images to accurately point the TIRS instrument to ensure that the products meet the TIRS-to-operational land imager (OLI) band registration and geometric accuracy requirements

  • Calibration have been automated to increase the quality of the real-time data provided to it provides scenes and process the imagery through the appropriate algorithm steps, and the user community

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Summary

Introduction

The Landsat 8 (L8) spacecraft was launched on 11 February, 2013 [1,2,3]. The spacecraft carries two payloads, the operational land imager (OLI) [4] and the thermal infrared sensor (TIRS) [5]. The TIRS instrument contains two thermal bands (10.6–11.2 μm and 11.5–12.5 μm), labeled as band 10 and band 11, respectively. These bands are made up of quantum well infrared photodetectors (QWIP).

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