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Mean Local Time of the Ascending Node

version 1.1 (370 KB) by

Determines the relationship between mean local time of the ascending node and RAAN.

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This geometric relationship defines the orientation of the spacecraft’s orbital plane with respect to the mean Sun. The MLTAN/RAAN relationship is important for mission design of sun-synchronous, repeating ground track, and other types of mission orbits that must satisfy Sun-orbit plane and other lighting constraints.

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Updates

1.1

Corrected annotation for raan2mltan.m function.

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MATLAB 7.14 (R2012a)

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