Analytical Solution of the Problem on an Axisymmetric Spacecraft Attitude Maneuver Optimal with Respect to a Combined Functional

Autor:	A. V. Molodenkov, Ya. G. Sapunkov
Rok vydání:	2021
Předmět:	Optimality criterion Spacecraft business.industry Rotational symmetry Conical surface Optimal control Rigid body Symmetry (physics) Constraint (information theory) Control and Systems Engineering Control theory Electrical and Electronic Engineering business Mathematics
Zdroj:	Automation and Remote Control. 82:1183-1200
ISSN:	1608-3032 0005-1179
DOI:	10.1134/s0005117921070043
Popis:	In the quaternionic setting, we consider the problem of optimal control of a spatial attitude maneuver of a spacecraft viewed as a rigid body with one symmetry axis without a constraint on the control function. For the optimality criterion we use a functional combining the time and energy spent on turning the spacecraft. Based on the Pontryagin maximum principle for this problem, new analytical solutions are obtained in the classes of conical and generalized conical motions. Numerical examples are given.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::90b241991674678ca5944ed6948824e2 https://doi.org/10.1134/s0005117921070043 Zobrazit plný text záznamu Plný text ve formátu PDF