Major refactoring and update of PUS module
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<p align="center"> <img src="misc/satrs-logo.png" width="40%"> </p>
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<p align="center"> <img src="misc/satrs-logo-v2.png" width="40%"> </p>
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[](https://absatsw.irs.uni-stuttgart.de/projects/sat-rs/)
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[](https://absatsw.irs.uni-stuttgart.de/projects/sat-rs/book/)
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@ -24,6 +24,11 @@ A lot of the architecture and general design considerations are based on the
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through the 2 missions [FLP](https://www.irs.uni-stuttgart.de/en/research/satellitetechnology-and-instruments/smallsatelliteprogram/flying-laptop/)
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and [EIVE](https://www.irs.uni-stuttgart.de/en/research/satellitetechnology-and-instruments/smallsatelliteprogram/EIVE/).
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This framework is in the early stages of development. Important features are missing. New releases
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with breaking changes are released regularly, with all changes documented inside respective
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changelog files. You should only use this framework if your are willing to work in this
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environment.
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# Overview
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This project currently contains following crates:
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@ -40,7 +45,7 @@ This project currently contains following crates:
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* [`satrs-mib`](https://egit.irs.uni-stuttgart.de/rust/sat-rs/src/branch/main/satrs-mib):
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Components to build a mission information base from the on-board software directly.
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* [`satrs-example-stm32f3-disco`](https://egit.irs.uni-stuttgart.de/rust/sat-rs/src/branch/main/satrs-example-stm32f3-disco):
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Example of a simple example on-board software using sat-rs components on a bare-metal system
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Example of a simple example using low-level sat-rs components on a bare-metal system
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with constrained resources.
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Each project has its own `CHANGELOG.md`.
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