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Near-Optimal Real-Time Spacecraft Guidance and Control Using Harmonic Potential Functions and a Modified RRT
By: Richard Zappulla II, Josep Virgili-Llop and Marcello Romano.
Pub. 2017,
19pgs.
PDF File.
AAS 17-420.
Price: $29.00
Reprinted from Advances in the Astronautical Sciences Spaceflight Mechanics 2017, volume 160.
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.