Parent Topic: AVHRCOR

DETAILS

AVHRCOR uses the NORAD SGP (Simplified General Perturbations) satellite orbital model. With this model, AVHRCOR performs a geometric correction using the following steps:

Step 1: Use the satellite name to locate the corresponding TLE (Two Line Element) file in either the current working directory, or $PCIHOME/etc. For example, the TLE file for the NOAA-12 satellite is called, noaa-12.2le. A TLE file contains orbital element values for a satellite at various epochs (dates).

Step 2: Locate the epoch in the TLE file which is closest to the approximate starting scan date. Extract the corresponding orbital element values. These orbital element values are used in satellite position/velocity prediction models. For best results, ensure that your TLE files are kept up-to-date. Ideally, the epoch date should not differ from the starting scan date by more than a few days.

Step 3: Given one GCP and an approximate starting scan date, use the satellite orbital model to compute the exact starting scan date. This process is referred to as image date refinement. Note that the GCP is only used to refine the image date. After image date refinement is performed, the mapping between pixel-line coordinates and geographic coordinates may still not match the GCP precisely. As a result a pixel-line shift is applied to ensure that the GCP is matched precisely. Note that image date refinement is only performed if the single GCP is available in the input file's text segment.

Image date refinement may fail in certain situations. If this occurs, the geometric correction cannot proceed. Possible reasons for image date refinement failure:

Step 4: Once the starting scan date is found, the transformations between the input image coordinates and the output image georeferencing system are fully determined. Every pixel in the output image is created by resampling the input image using these transformations.


Parent Topic: AVHRCOR
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