Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters

Gespeichert in:
Bibliographische Detailangaben
Datum:2017
1. Verfasser: N. V. Efimenko
Format: Artikel
Sprache:English
Veröffentlicht: 2017
Schriftenreihe:International Scientific Technical Journal «Problems of Control and Informatics»
Online Zugang:http://jnas.nbuv.gov.ua/article/UJRN-0001286305
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Назва журналу:Library portal of National Academy of Sciences of Ukraine | LibNAS

Institution

Library portal of National Academy of Sciences of Ukraine | LibNAS
id open-sciencenbuvgovua-45806
record_format dspace
spelling open-sciencenbuvgovua-458062024-02-29T12:11:30Z Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters N. V. Efimenko 2786-6491 2017 en International Scientific Technical Journal «Problems of Control and Informatics» http://jnas.nbuv.gov.ua/article/UJRN-0001286305 Article
institution Library portal of National Academy of Sciences of Ukraine | LibNAS
collection Open-Science
language English
series International Scientific Technical Journal «Problems of Control and Informatics»
spellingShingle International Scientific Technical Journal «Problems of Control and Informatics»
N. V. Efimenko
Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
format Article
author N. V. Efimenko
author_facet N. V. Efimenko
author_sort N. V. Efimenko
title Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
title_short Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
title_full Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
title_fullStr Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
title_full_unstemmed Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
title_sort synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at rodrigues–hamilton parameters
publishDate 2017
url http://jnas.nbuv.gov.ua/article/UJRN-0001286305
work_keys_str_mv AT nvefimenko synthesisoftimeoptimalthreedimensionalrotationofspacecraftusingrotationalmotionofequationofrigidbodyatrodrigueshamiltonparameters
first_indexed 2025-07-17T21:12:17Z
last_indexed 2025-07-17T21:12:17Z
_version_ 1850415971387310080