Analytical solution of the time-optimal slew problem of a spherically symmetric spacecraft in the class of conical motions

DOI10.1134/S1064230714020130zbMath1311.49005OpenAlexW2566095235MaRDI QIDQ2263885

Publication date: 19 March 2015

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

Full work available at URL: https://doi.org/10.1134/s1064230714020130

zbMATH Keywords

analytical solution Pontryagin's maximum principle conical motions spherically symmetric spacecraft time-optimal slew problem

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Existence theories for optimal control problems involving ordinary differential equations (49J15) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (7)

Analytical approximate solution of the problem of a spacecraft's optimal turn with arbitrary boundary conditions ⋮ Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional ⋮ Statistical analysis of diffusion systems with invariants ⋮ Electrodynamic stabilization of artificial Earth satellites in the König coordinate system ⋮ Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft ⋮ 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

Cites Work

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