Special control regime in the problem of optimal turn of an axially symmetric spacecraft

DOI10.1134/S1064230710060079zbMath1269.49081OpenAlexW1987746955MaRDI QIDQ2391519

Ya. G. Sapunkov, A. V. Molodenkov

Publication date: 31 July 2013

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230710060079

zbMATH Keywords

axially symmetric spacecraft, optimal turnspecial control regime

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (3)

Optimal control of a spacecraft orientation taking into account the energy of rotation ⋮ Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft) ⋮ Analytic controlling reorientation of a spacecraft using a combined criterion of optimality

Cites Work

• Unnamed Item
• A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
• Special control regime in optimal turn problem of spherically symmetric spacecraft
• A shooting method for solving two-point boundary-value problems arising from non-singular bang-bang optimal control problems

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