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Problem "Messenger-Full" (MGA-1DSM) This trajectory optimisation problem represents a rendezvous mission to Mercury modelled as an MGA-1DSM problem. It includes the final resonant fly-bys, and seeks to minimse the on-board propellant consumption. |
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Short description This trajectory optimisation problem represents a rendezvous mission to Mercury modelled as an MGA-1DSM problem. The selected fly-by sequence and other parameters are compatible with the currently flying Messenger mission. With respect to the problem "Messenger" the fly-by sequence is more complex and allows for resonant fly-bys at Mercury to lower the arrival DV. For the twenty-six dimensional global optimisation problem we consider the bounds listed in the following table:
No other constraints are considered for this problem. The objective function is considered to the precision of meters per second. | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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