Saltar navegación principal
Normas DIN – AENOR
DIN EN 16603-60-30:2014-09

DIN EN 16603-60-30:2014-09

Space engineering - Satellite AOCS requirements; English version FprEN 16603-60-30:2014 / Note: Date of issue 2014-08-15

Ingénierie spatiale - Exigences pour le système de contrôle d'attitude et d'orbite d'un satellite; Version anglaise FprEN 16603-60-30:2014 / Attention: Date de parution 2014-08-15

Raumfahrttechnik - Anforderungen an Satelliten-AOCS; Englische Fassung FprEN 16603-60-30:2014 / Achtung: Erscheinungsdatum 2014-08-15

Fecha Anulación:
2015-12 /Withdrawn
Equivalencias internacionales:

FprEN 16603-60-30 (2014-05)

Relación con otras normas DIN:

Reemplazada por: DIN EN 16603-60-30:2015-12

Resumen:
This Standard specifies a baseline for the attitude and orbit control system requirements to be used in the Project Requirements Document for space applications. Project requirements documents are included in business agreements, which are agreed between the parties and binding them, at any level of space programmes, as described in ECSS-S-ST-00. This Standard deals with the attitude and orbit control systems developed as part of a satellite space project. The classical attitude and orbit control systems considered here include the following functions: - Attitude estimation - Attitude guidance - Attitude control - Orbit control - Orbit estimation, called Navigation in this document, can be part of the function for missions which explicitly require this function - Acquisition and maintenance of a safe attitude in emergency cases and return to nominal mission upon commandThe present Standard does not cover missions that include the following functions: - Real-time on-board trajectory guidance and control - Real-time on-board relative position estimation and controlExample of such missions are rendezvous, formation flying, launch vehicles and interplanetary vehicles.Although the present document does not cover the above mentioned types of mission, it can be used as a reference document for them.This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.
Keywords:
Aerospace transport, Definitions, Flight operations, Flight performance, Functionality, Orbit, Outer space, Performance requirements, Quality, Satellites, Space safety, Space technology, Space transport, Specification (approval), Telemetry, Terminology, Verification
119,63
Idioma Formato

Formato digital

Nota: Precios sin IVA ni gastos de envío

Añadir a la cesta