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

DOI10.1134/S0005117917120086zbMath1388.49051OpenAlexW2775369063MaRDI QIDQ2412971

I. A. Danilina, I. S. Grigoriev

Publication date: 6 April 2018

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

Full work available at URL: https://doi.org/10.1134/s0005117917120086

zbMATH Keywords

Pontryagin's maximum principletrajectory optimizationspace vehicleadditional fuel tank

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Geodesy, mapping problems (86A30) Geophysics (86A99) Variational principles of physics (49S05)

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• A survey of methods available for the numerical optimization of continuous dynamic systems
• Optimization of interorbital three-dimensional transfer trajectories for stage spacecraft
• Optimal control of a system with intermediate conditions
• Numerical solution of boundary-value problems of the maximum principle in optimization space flight dynamics problem
• Optimal control problems for equations with discontinuous right-hand sides
• Optimal control of stepped systems
• Variational problems of optimization of control processes for equations with discontinuous right-hand sides
• Necessary conditions of the calculus of variations for a problem of bolza-mayer type
• Sufficient conditions for the absolute extremum in a variational problem of the bolza — meyer type
• Optimization of motion for a two-stage rocket
• On a type of variational problems

This page was built for publication: Optimizing flight trajectories for space vehicles with an additional fuel tank. I