Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming

DOI10.1007/S10569-009-9224-3zbMath1223.70076OpenAlexW2047377127MaRDI QIDQ642298

Camilla Colombo, Gianmarco Radice, Massimiliano Vasile

Publication date: 26 October 2011

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://strathprints.strath.ac.uk/18838/

zbMATH Keywords

optimal controlasteroidsdifferential dynamic programmingoptimisation methods\(N\)-bodyBellman principlelow-thrust trajectoriesmulti-body problemmulti-revolution trajectorynear-Earth objectsrendez-vous trajectory to Apophistrajectory optimisation

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Control of mechanical systems (70Q05) Orbital mechanics (70M20) (n)-body problems (70F10)

Related Items (4)

A continuous implementation of a second-variation optimal control method for space trajectory problems ⋮ A hybrid differential dynamic programming algorithm for constrained optimal control problems. I: Theory ⋮ A hybrid differential dynamic programming algorithm for constrained optimal control problems. II: Application ⋮ On the deflection of asteroids with mirrors

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