Micro satellite on-orbit reconstruction frame system and method
A framework system and micro-satellite technology, applied in the aerospace field, can solve problems such as the inability to effectively meet the demand changes in the later stage of satellite development or during the orbit, and the software adaptability is weak, and achieve the effect of improving software adaptability and meeting demand changes.
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[0040] Example 1:
[0041] like figure 1 Shown is a satellite on-orbit reconstruction framework system provided by an embodiment of the present invention. The system includes an application layer, a system interface layer, and a port driver layer, wherein:
[0042] The application layer includes a plurality of application layer modules, and each application layer module has a standardized external interface; the specific interfaces include: an initialization interface, a module instruction processing interface and a module main program interface; wherein: the initialization interface is responsible for the initialization module; the instruction processing interface The interface is responsible for processing module-related instructions; the main program of the module completes the actual function of the module.
[0043] The port driver layer includes a plurality of external software and hardware interface modules, each external software and hardware interface module has a sta...
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[0051] Embodiment 2:
[0052] The satellite on-orbit reconstruction framework method provided by the second embodiment of the present invention is based on the satellite on-orbit reconstruction framework system, and the system includes an application layer, a system interface layer and a port driver layer, wherein:
[0053] The application layer includes a plurality of application layer modules, the application layer modules can be used to complete various specific functions of the onboard software, and each application layer module has a standardized external interface;
[0054] The system interface layer includes a core scheduling layer, a data exchange layer, a first interface form and a second interface form; wherein: the first interface form stores the normalized external interface address and each parameter address of each application layer module; The second interface form stores the normalized external interface address of each port driver layer module; the core schedu...
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