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The main objective of the project was to select the right IMU for our Future GNSS Receiver Unit (GRU). Two IMU were selected from their datasheet : µ-UMI-IC-HP from Litef and STIM318 from Sensonor. These 2 IMU were submitted to hard characterization tests applicable to our Launchers (and
HAPS) application.
THALES ALENIA SPACE...
- Enforce the use of the physical engineering model that TAS-F already has by sub-system architects in order to have the model as a central source of truth
- Produce an interactive representation of the model allowing its consultation without having to install dedicated modelling tools
- Produce trend graphs on system budgets
- Produce document generation capability to export graphs and tables to the system and subsystem budget reports
Thales Alenia Space
This study aimed to achieve the following objectives:
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To anticipate the security needs and requirements of future space missions (Earth observation, communication, navigation, science, exploration, etc.) with respect to architectures considered for future missions.
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To build an advanced security architecture portfolio embedding state-of-the-art security concepts, technics, technologies, components and solutions.
Thales Alenia Space
Currently employed approaches to FDIR development are poorly phased with regard to the main Software Development activities. They have tendency of starting late, awaiting for the system Failure Mode Effects and Criticality Analysis (FMECA) data. If functional FMECA is sometimes available, its update into the physical FMECA is seldom ready for software development. FDIR definition is not adequately synchronised with the nominal Software System behaviour.
THALES ALENIA SPACE...
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