EN 16603-50-03:2014
(Main)Space engineering - Space data links - Telemetry transfer frame protocol
Space engineering - Space data links - Telemetry transfer frame protocol
This Standard contains the definition for Telemetry Transfer Frames which are fixed-length data structures, suitable for transmission at a constant frame rate on a space data channel.
The Telemetry Transfer Frame provides a standardized data structure for the transmission of space-acquired data over a telemetry space data link.
Usually, the source of the data is located in space and the receiver is located on the ground. However, this Standard may also be applied to space-to-space telemetry data links.
Further provisions and guidance on the application of this standard can be found, respectively, in the following publications:
- The higher level standard ECSS-E-ST-50, Communications, which defines the principle characteristics of communication protocols and related services for all communication layers relevant for space communication (physical- to application-layer), and their basic relationship to each other.
- The handbook ECSS-E-HB-50, Communications guidelines, which provides information about specific implementation characteristics of these protocols in order to support the choice of a certain communications profile for the specific requirements of a space mission..
Users of this present standard are invited to consult these documents before taking decisions on the implementation of the present one.
This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Raumfahrttechnik - Raumfahrt-Datenübertragung - Telemetrieübertragungs-Rahmen-Protokoll
Ingénierie spatiale - Liaisons des données spatiales - Protocole trame de transfert de télémesure
La présente norme contient la définition des trames de transfert de télémesure, qui sont des structures de données de longueur fixe, convenant à la transmission de trames à vitesse constante via un canal de données spatial.
La Trame de Transfert de Télémesure fournit une structure de données normalisée permettant de transmettre des données acquises dans l'espace via une liaison spatiale de données de télémesure.
En règle générale, la source des données est située dans l'espace et le récepteur se trouve au sol. Toutefois, la présente norme peut également être appliquée aux liaisons de données de télémesure entre engins spatiaux.
Les publications suivantes contiennent, respectivement, des dispositions et des préconisations supplémentaires concernant l'application de la présente norme :
• la norme mère ECSS-E-ST-50, « Communications », qui définit les principes des protocoles de communication et des services connexes pour toutes les couches de communication spatiale (de la couche physique à la couche applicative), et décrit leurs relations de base ;
• le manuel ECSS-E-HB-50, « Communications guidelines », qui fournit des informations sur les caractéristiques de mise en œuvre de ces protocoles afin d'orienter le choix d'un profil de communication donné compte tenu des exigences particulières d'une mission spatiale.
Les utilisateurs de la présente norme sont invités à consulter ces documents avant de prendre toute décision quant à sa mise en œuvre.
La présente norme peut être adaptée aux caractéristiques et contraintes spécifiques d'un projet spatial, conformément à la norme ECSS-S-ST-00.
Vesoljska tehnika - Vesoljske podatkovne povezave - Okvirni protokol za prenos telemetrijskih podatkov
Ta standard vsebuje definicijo za okvire prenosa telemetrijskih podatkov, ki so podatkovne strukture fiksne dolžine, primerne za prenos pri stalni hitrosti na vesoljskem podatkovnem kanalu.
Okvir prenosa telemetrijskih podatkov zagotavlja standardizirano podatkovno strukturo za prenos v vesolju pridobljenih podatkov prek telemetrijske vesoljske podatkovne povezave.
Običajno se vir podatkov nahaja v vesolju, sprejemnik pa se nahaja na tleh. Vendar se lahko ta standard uporablja tudi za telemetrijske podatkovne povezave v vesolju.
Dodatne določbe in smernice o uporabi tega standarda je mogoče najti v naslednjih publikacijah:
– v standardu višje ravni ECSS-E-ST-50 (Komunikacije), ki določa glavne značilnosti komunikacijskih protokolov in z njimi povezanih storitev za vse ravni komunikacije, pomembne za vesoljsko komunikacijo (od fizične do aplikacijske ravni), in njihove osnovne medsebojne povezave,
– v priročniku ECSS-E-HB-50 (Komunikacijske smernice), ki zagotavlja informacije o posebnih značilnostih vpeljave teh protokolov za podporo pri izbiri določenega komunikacijskega profila za posebne zahteve vesoljske misije.
Uporabniki obstoječega standarda so vabljeni k ogledu teh dokumentov, preden sprejmejo odločitve o izvajanju trenutnega standarda.
Ta standard se lahko prilagodi posameznim lastnostim in omejitvam vesoljskega projekta v skladu s standardom ECSS-S-ST-00.
General Information
Relations
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Vesoljska tehnika - Vesoljske podatkovne povezave - Okvirni protokol za prenos telemetrijskih podatkovRaumfahrttechnik - Telemetrieübertragungs-Rahmen-ProtokollIngénierie spatiale - Liaisons des données spatiales - Protocole trame de transfert de télémesureSpace engineering - Space data links - Telemetry transfer frame protocol49.140Vesoljski sistemi in operacijeSpace systems and operations33.200Daljinsko krmiljenje, daljinske meritve (telemetrija)Telecontrol. TelemeteringICS:Ta slovenski standard je istoveten z:EN 16603-50-03:2014SIST EN 16603-50-03:2015en01-januar-2015SIST EN 16603-50-03:2015SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 16603-50-03
September 2014 ICS 49.140
English version
Space engineering - Space data links - Telemetry transfer frame protocol
Ingénierie spatiale - Liaisons des données spatiales - Protocole trame de transfert de télémesure
Raumfahrtproduktsicherung - Telemetrieübertragungs-Rahmen-Protokoll This European Standard was approved by CEN on 11 April 2014.
CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN and CENELEC member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN and CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions.
CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.
CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels © 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16603-50-03:2014 E SIST EN 16603-50-03:2015
Tables Table 5-1: Major fields in a TM Transfer Frame . 11 Table B-1: Differences in names from ESA-PSS-04-106 for fields in a Telemetry Transfer Frame . 35 Table B-1 : Differences in names from ESA-PSS-04-106 for fields in a Telemetry Transfer Frame . 35
Usually, the source of the data is located in space and the receiver is located on the ground. However, this Standard may also be applied to space-to-space telemetry data links.
Further provisions and guidance on the application of this standard can be found, respectively, in the following publications:
• The higher level standard ECSS-E-ST-50, Communications, which defines the principle characteristics of communication protocols and related services for all communication layers relevant for space communication (physical- to application-layer), and their basic relationship to each other.
• The handbook ECSS-E-HB-50, Communications guidelines, which provides information about specific implementation characteristics of these protocols in order to support the choice of a certain communications profile for the specific requirements of a space mission. Users of this present standard are invited to consult these documents before taking decisions on the implementation of the present one. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. SIST EN 16603-50-03:2015
EN reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01 ECSS system – Glossary of terms EN 16603-50-01 ECSS-E-ST-50-01 Space engineering – Space data links – Telemetry synchronization and channel coding EN 16603-50-04 ECSS-E-ST-50-04 Space engineering – Space data links – Telecommand protocols, synchronization and channel coding
CCSDS 133.0-B-1
Space Packet Protocol – Blue Book, Issue 1, September 2003
CCSDS 135.0-B-3
Space Link Identifiers – Blue Book, Issue 3, October 2006
The bit pattern of idle data is not specified. 3.2.2 mission phase period of a mission during which specified telemetry characteristics are fixed NOTE
The transition between two consecutive mission phases can cause an interruption of the telemetry services. 3.2.3 octet group of eight bits NOTE 1 The numbering for octets within a data structure starts with 0. NOTE 2 Refer to clause 3.4 for the convention for the numbering of bits. 3.2.4 packet variable-length data structure consisting of higher layer user data encapsulated within standard header information 3.2.5 static unchanged within a specific virtual channel or within a specific master channel NOTE
This Standard contains requirements on the invariability, throughout one or all mission phases, of certain characteristics of the data structures specified in it. SIST EN 16603-50-03:2015
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