Tracking and impact point of survey rocket by Telemetry and Slant-Range device
Autor(a) principal: | |
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Data de Publicação: | 2022 |
Outros Autores: | , , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Anais da Academia Brasileira de Ciências (Online) |
Texto Completo: | http://old.scielo.br/scielo.php?script=sci_arttext&pid=S0001-37652022000501708 |
Resumo: | Abstract This work presents an alternative method of getting tracking, and the impact point of the actual flight of a rocket, by telemetry data and slant-range device. The tracking and impact point data were obtained from an actual flight path by merging the angular components of a telemetry antenna (Azimuth, and Elevation) and the radial distance information provided by the slant-range device. The position components were analyzed with the telemetry antenna in automatic mode, target tracking, comparing with the tracking results performed by the radar. The result obtained by the composition of the coordinates of the telemetry/slant-range set, it was observed that the point of impact generated by this group had a distance of 237.64 (meters), in relation to the impact generated by the tracking of the radar. Indicating a significant reduction of the search area and can be used as na alternative form of use. It allows you to provide additional location information for payload recovery around the actual point of impact. |
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Anais da Academia Brasileira de Ciências (Online) |
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Tracking and impact point of survey rocket by Telemetry and Slant-Range deviceImpact pointrocketslant-range devicetelemetrytrackingAbstract This work presents an alternative method of getting tracking, and the impact point of the actual flight of a rocket, by telemetry data and slant-range device. The tracking and impact point data were obtained from an actual flight path by merging the angular components of a telemetry antenna (Azimuth, and Elevation) and the radial distance information provided by the slant-range device. The position components were analyzed with the telemetry antenna in automatic mode, target tracking, comparing with the tracking results performed by the radar. The result obtained by the composition of the coordinates of the telemetry/slant-range set, it was observed that the point of impact generated by this group had a distance of 237.64 (meters), in relation to the impact generated by the tracking of the radar. Indicating a significant reduction of the search area and can be used as na alternative form of use. It allows you to provide additional location information for payload recovery around the actual point of impact.Academia Brasileira de Ciências2022-01-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S0001-37652022000501708Anais da Academia Brasileira de Ciências v.94 n.3 2022reponame:Anais da Academia Brasileira de Ciências (Online)instname:Academia Brasileira de Ciências (ABC)instacron:ABC10.1590/0001-3765202220200471info:eu-repo/semantics/openAccessCANTANHEDE,NILTON R.CARVALHO,EWALDO EDERSILVA JÚNIOR,PAULO FERNANDES DABARROS,JONAS DE JESUSeng2022-11-03T00:00:00Zoai:scielo:S0001-37652022000501708Revistahttp://www.scielo.br/aabchttps://old.scielo.br/oai/scielo-oai.php||aabc@abc.org.br1678-26900001-3765opendoar:2022-11-03T00:00Anais da Academia Brasileira de Ciências (Online) - Academia Brasileira de Ciências (ABC)false |
dc.title.none.fl_str_mv |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
title |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
spellingShingle |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device CANTANHEDE,NILTON R. Impact point rocket slant-range device telemetry tracking |
title_short |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
title_full |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
title_fullStr |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
title_full_unstemmed |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
title_sort |
Tracking and impact point of survey rocket by Telemetry and Slant-Range device |
author |
CANTANHEDE,NILTON R. |
author_facet |
CANTANHEDE,NILTON R. CARVALHO,EWALDO EDER SILVA JÚNIOR,PAULO FERNANDES DA BARROS,JONAS DE JESUS |
author_role |
author |
author2 |
CARVALHO,EWALDO EDER SILVA JÚNIOR,PAULO FERNANDES DA BARROS,JONAS DE JESUS |
author2_role |
author author author |
dc.contributor.author.fl_str_mv |
CANTANHEDE,NILTON R. CARVALHO,EWALDO EDER SILVA JÚNIOR,PAULO FERNANDES DA BARROS,JONAS DE JESUS |
dc.subject.por.fl_str_mv |
Impact point rocket slant-range device telemetry tracking |
topic |
Impact point rocket slant-range device telemetry tracking |
description |
Abstract This work presents an alternative method of getting tracking, and the impact point of the actual flight of a rocket, by telemetry data and slant-range device. The tracking and impact point data were obtained from an actual flight path by merging the angular components of a telemetry antenna (Azimuth, and Elevation) and the radial distance information provided by the slant-range device. The position components were analyzed with the telemetry antenna in automatic mode, target tracking, comparing with the tracking results performed by the radar. The result obtained by the composition of the coordinates of the telemetry/slant-range set, it was observed that the point of impact generated by this group had a distance of 237.64 (meters), in relation to the impact generated by the tracking of the radar. Indicating a significant reduction of the search area and can be used as na alternative form of use. It allows you to provide additional location information for payload recovery around the actual point of impact. |
publishDate |
2022 |
dc.date.none.fl_str_mv |
2022-01-01 |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S0001-37652022000501708 |
url |
http://old.scielo.br/scielo.php?script=sci_arttext&pid=S0001-37652022000501708 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
10.1590/0001-3765202220200471 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
text/html |
dc.publisher.none.fl_str_mv |
Academia Brasileira de Ciências |
publisher.none.fl_str_mv |
Academia Brasileira de Ciências |
dc.source.none.fl_str_mv |
Anais da Academia Brasileira de Ciências v.94 n.3 2022 reponame:Anais da Academia Brasileira de Ciências (Online) instname:Academia Brasileira de Ciências (ABC) instacron:ABC |
instname_str |
Academia Brasileira de Ciências (ABC) |
instacron_str |
ABC |
institution |
ABC |
reponame_str |
Anais da Academia Brasileira de Ciências (Online) |
collection |
Anais da Academia Brasileira de Ciências (Online) |
repository.name.fl_str_mv |
Anais da Academia Brasileira de Ciências (Online) - Academia Brasileira de Ciências (ABC) |
repository.mail.fl_str_mv |
||aabc@abc.org.br |
_version_ |
1754302872464392192 |