Published July 3, 2019
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Equations for General Perturbation Method for Satellite Constellation Reconfiguration Using Low-Thrust Maneuvers
Description
Equations from the paper General Perturbation Method for Satellite Constellation Reconfiguration Using Low-Thrust Maneuvers published in the AIAA Journal of Guidance, Control, and Dynamics.
The equations are provided in forms suitable for use in Wolfram Mathematica (.nb), Matlab (.m) and Python (.py).
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Additional details
Related works
- Is supplement to
- Journal article: 10.2514/1.G003739 (DOI)