Optimizing flight trajectories for space vehicles with an additional fuel tank. II

DOI10.1134/S0005117918020108zbMath1390.49015OpenAlexW4232477001WikidataQ130170314 ScholiaQ130170314MaRDI QIDQ1642042

I. A. Danilina, I. S. Grigoriev

Publication date: 20 June 2018

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0005117918020108

zbMATH Keywords

spacecraftPontryagin's maximum principletrajectory optimizationauxiliary fuel tank

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Control problems involving ordinary differential equations (34H05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (1)

Fixed Point Methods for Solving Boundary Value Problem of the Maximum Principle

Cites Work

• Optimization of interorbital three-dimensional transfer trajectories for stage spacecraft

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