Research Article

Numerical Validation of the Delaunay Normalization and the Krylov-Bogoliubov-Mitropolsky Method

Figure 6

Box and whisker plots for DN and KBM orbital element errors with for a time span of 7 days.
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(a) Semimajor axis errors
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(b) Eccentricity errors
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(c) Inclination errors
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(d) Argument of the perigee errors