Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions

DOI10.1134/S1064230716060095zbMath1387.49058MaRDI QIDQ1743200

A. V. Molodenkov, Ya. G. Sapunkov

Publication date: 13 April 2018

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

zbMATH Keywords

axisymmetric spacecraftminimum energy costsoptimal spacecraft slew

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (5)

Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions ⋮ Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional ⋮ Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions ⋮ Optimal control of rigid body's rotation movement with a combined quality criterion ⋮ Analytical quasi-optimal solution of the slew problem for an axially symmetric rigid body with a combined performance index

Cites Work

• Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions
• Analytical approximate solution of the problem of a spacecraft's optimal turn with arbitrary boundary conditions
• Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
• A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
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