Optimization of space vehicle manoeuvre between planetocentric elliptical orbit and the sphere of influence

zbMATH Open1249.49029MaRDI QIDQ2897423

O. T. Dekhtyar, O. Kharytonov

Publication date: 16 July 2012

Published in: Visnyk. Seriya: Fizyko-Matematychni Nauky. Kyïvs'kyĭ Universytet Imeni Tarasa Shevchenka (Search for Journal in Brave)

zbMATH Keywords

Pontryagin's maximum principletrajectory optimizationfinite-thrustinterplanetary transfer

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (2)

Optimal spatial launch of a spacecraft into a geostationary orbit from and artificial satellite orbit ⋮ Method of optimizing maneuvers of an orbital transfer vehicle in a strong central field of gravity

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