Analytical Solution of Equations of Near-circular Spacecraft’s Orbit Orientation

DOI10.18500/1816-9791-2015-15-1-97-105zbMATH Open1326.70048OpenAlexW3094161784MaRDI QIDQ3453934

Il'Ya Alekseevich Pankratov

Publication date: 1 December 2015

Published in: Izvestiya of Saratov University. New Series. Series: Mathematics. Mechanics. Informatics (Search for Journal in Brave)

Full work available at URL: http://mathnet.ru/eng/isu570

zbMATH Keywords

optimal controlorbitspacecraftorientationquaternion

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (3)

Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions ⋮ Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions ⋮ Symbolic-analytic methods for studying equilibrium orientations of a satellite on a circular orbit

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