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Describe your use case
This module implements target point for a spacecraft with rotating solar arrays. This module computes a reference attitude that aligns a desired body-fixed axis with the direction of a celestial body. Roll about the alignment axis is used to maximize the incidence on the solar arrays.
Describe alternatives solutions you've considered
N/A
Additional context
N/A
The text was updated successfully, but these errors were encountered:
Describe your use case
This module implements target point for a spacecraft with rotating solar arrays. This module computes a reference attitude that aligns a desired body-fixed axis with the direction of a celestial body. Roll about the alignment axis is used to maximize the incidence on the solar arrays.
Describe alternatives solutions you've considered
N/A
Additional context
N/A
The text was updated successfully, but these errors were encountered: