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No-guess indirect optimization of asteroid mission using electric propulsion

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Publication:3176487
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DOI10.1002/oca.2396zbMath1391.93157OpenAlexW2781778817MaRDI QIDQ3176487

HongXin Shen

Publication date: 20 July 2018

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.2396


zbMATH Keywords

optimal controltrajectory optimizationindirect methodasteroid mission


Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Automated systems (robots, etc.) in control theory (93C85) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)


Related Items (2)

A mesh refinement method for low‐thrust orbit transfer problems ⋮ A fast computational method for the minimum duration transfer trajectories of space-to-ground vehicles






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