Optimal guidance for quasi-planar lunar ascent

DOI10.1007/s10957-011-9884-5zbMath1251.49052OpenAlexW2057090670MaRDI QIDQ658554

David G. Hull

Publication date: 12 January 2012

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10957-011-9884-5

zbMATH Keywords

optimal controloptimal guidancelunar ascent

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control problems involving ordinary differential equations (34H05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items

Second order necessary and sufficient optimality conditions for singular solutions of partially-affine control problems, Maximum divert for planetary landing using convex optimization, Optimal low-thrust orbital maneuvers via indirect swarming method

Cites Work

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