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A New Methodology for the Solution of the Stiffness Problem Applied to Low- Thrust Trajectory Optimisation in Terms of Orbital Elements Using Differential Dynamic Programming
By: Marco Nugnes and Camilla Colombo.
Pub. 2021, 16pgs.
PDF File. AAS 21-369.
Price: $29.00
 

Reprinted from Advances in the Astronautical Sciences AAS/AIAA Spaceflight Mechanics 2021, volume 176

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