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Journal of Computer and Systems Sciences International
Erschienen in: Journal of Computer and Systems Sciences International 3/2023

01.10.2023 | CONTROL SYSTEMS FOR MOVING OBJECTS

Analytical Quasi-Optimal Algorithm for the Programmed Control of the Angular Motion of a Spacecraft

verfasst von: A. V. Molodenkov, I. G. Sapunkov

Erschienen in: Journal of Computer and Systems Sciences International | Ausgabe 3/2023

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Abstract

The problem of the optimal program control of the angular motion of a spacecraft (SC) as a rigid body with a quadratic functional of the energy spent on the maneuver of the SC and a fixed time of the transition process is investigated. The dynamic configuration of the SC and the boundary conditions are arbitrary and the control vector function is not limited. In the Poinsot concept, using the Pontryagin maximum principle, a quasi-optimal analytical solution of the problem is obtained, which is developed into an algorithm. Confirming numerical examples are given, showing the proximity of the quasi-optimal solution to the optimal solution of the problem.
Vorheriger Artikel Generalization of the Rutherford Formula and Synthesis of Trajectories with Gravity Assist Maneuvers
Nächster Artikel Optimal Control of the Reorientation of a Spacecraft in the Given Time with a Quadratic Performance Criterion Related to the Control and Phase Variables

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Metadaten
Titel
Analytical Quasi-Optimal Algorithm for the Programmed Control of the Angular Motion of a Spacecraft
verfasst von
A. V. Molodenkov
I. G. Sapunkov
Publikationsdatum
01.10.2023
Verlag
Pleiades Publishing
Erschienen in
Journal of Computer and Systems Sciences International / Ausgabe 3/2023
Print ISSN: 1064-2307
Elektronische ISSN: 1555-6530
DOI
https://doi.org/10.1134/S1064230723030103

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