IEEE Transactions on Geoscience and Remote Sensing · 2007 · 101 citations · 10 references
Natural SciencesAerospace EngineeringEarth SciencesGeodesyGlobal Navigation Satellite SystemsRemote SensingAttitude DeterminationGeometric CorrectionInfrared Remote SensingRemote Sensing ImagerySatellite InstrumentationSatellite SensorsGeometric Correction Of Satellite ImageryImage Distortion CorrectionImage Distortion ReductionRegistrationRegistration Error ReductionRemote Sensing SystemsSpacecraft Attitude ErrorsSpacecraft Attitude Estimation
Accurate attitude estimation of spacecrafts is the main requirement to provide good geometric performance of remote-sensing imagery. The Advanced Spaceborne Thermal Emission and Reflection Radiometer/short-wave-infrared subsystem has six linear-array sensors arranged in parallel, and each line scans the same ground target with a time interval of 356.238 ms between neighboring bands. The registration performance between bands becomes worse when attitude fluctuation occurs during a time lag between observations. Since the time resolution of the line scan is higher than that of the attitude information provided from the satellite, attitude data are estimated with a high frequency. We succeeded in correcting the image-registration error using the revised attitude information. As a result, the image distortion of 0.2 pixels caused by spacecraft-attitude jitter is reduced to less than 0.08 pixels, showing that band-to-band registration errors of a sensor with parallax observation are available to improve the image distortion caused by attitude fluctuation.
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