The direct transcription method has been used to solve many challenging optimal control problems. One such example involves the calculation of a low thrust orbit transfer between libration point orbits. The recent implementation of high order discretization techniques is first described and then illustrated by computing optimal low thrust trajectories between orbits about the L1 and L2 Earth-Moon libration points.
Using Direct Transcription to Compute Optimal Low Thrust Transfers Between Libration Point Orbits
Springer Optimization
01.01.2017
38 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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