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

In this paper an optimisation algorithm based on Differential dynamic programming is applied to the design of rendezvous and fly-by trajectories to near Earth objects. Differential dynamic programming is a successive approximation technique that computes a feedback control law in correspondence of a...

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Veröffentlicht in:	Celestial mechanics and dynamical astronomy 2009-11, Vol.105 (1-3), p.75-112
Hauptverfasser:	Colombo, Camilla, Vasile, Massimiliano, Radice, Gianmarco
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Technology and Astronautics Algorithms Asteroids Astrophysics and Astroparticles Classical Mechanics Dynamic programming Dynamical Systems and Ergodic Theory Geophysics/Geodesy Original Article Physics Physics and Astronomy Space exploration Spacecraft
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