摘要(英) |
This thesis aims to develop space weather science instrument payload including ontology system(engineering model and flying model) and development system(program model), hoping to complete the system stability and high reliability of weather science measurement applications.
Ontology system of the space weather science instrument payload integrates digital signal processing unit, DC/DC power supply system and the following five scientific instruments system: magneto-resistive magnetometer sub-system, separate Magneto-Resistive magnetometer sub-system, plasma electron temperature and density probe sub-system, airglow photo-tomograph instrument sub-system, gravity and gyro sensing sub-system. Using the space weather data measured by the instrument, we expect to analyze the clues relating to space weather changes.
In order to ensure the accuracy of the information and the stability of the scientific instruments payload, this thesis construct a scientific instrument payload development system that integrates multiple development platform and testing platform. The development system can help the scientific instrument payload on the mission requirements for functionality and performance verification. I hope the space weather science instrument payload, whether the objectives and functions of the design of hardware or firmware can be really stable implementation of the tasks set.
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參考文獻 |
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