DocumentCode :
279870
Title :
Application specific spacecraft
Author :
Brown, J. E E
Author_Institution :
MSS Ltd., Salford, UK
fYear :
1990
fDate :
32962
Firstpage :
42552
Lastpage :
42555
Abstract :
Describes the design of a small satellite, named Innovative Modular Satellite (IMS), which resulted from a study conducted by MSS Ltd for the European Space Agency (ESA). The unique feature of the IMS system architecture is the collection of all service control functions within a single subsystem, the control subsystem, rather than the conventional architecture where control is spread throughout all the subsystems. This has advantages in that duplication of hardware is avoided and the overall control complexity is minimised with a consequent improvement in reliability and a reduction in software cost. This approach is facilitated on the IMS by the centralisation of most of the onboard service electronics in a single Service Electronics Rack (SER) and the intention to adopt a single source procurement philosophy at electrical system level
Keywords :
satellite relay systems; telecommunications computer control; ESA; European Space Agency; Innovative Modular Satellite; MSS Ltd; Service Electronics Rack; application specific spacecraft; control subsystem; electrical system; onboard service electronics; reliability; service control functions; small satellite; software cost; system architecture;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Earth Resource Sensing and the Data Relay Satellite, IEE Colloquium on
Conference_Location :
London
Type :
conf
Filename :
189937
Link To Document :
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