update rust book as well
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@ -15,7 +15,7 @@ action commanding could look like.
2. Target ID and Action String based. The target ID is the same as in the first proposal, but
the unique action is identified by a string.
The framework provides an `ActionRequest` abstraction to model both of these cases.
The library provides an `ActionRequest` abstraction to model both of these cases.
## Commanding with ECSS PUS 8

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@ -20,7 +20,7 @@ components.
1. [UDP TMTC Server](https://docs.rs/satrs/latest/satrs/hal/host/udp_server/index.html).
UDP is already packet based which makes it an excellent fit for exchanging space packets.
2. [TCP TMTC Server Components](https://docs.rs/satrs/latest/satrs/hal/std/tcp_server/index.html).
TCP is a stream based protocol, so the framework provides building blocks to parse telemetry
TCP is a stream based protocol, so the library provides building blocks to parse telemetry
from an arbitrary bytestream. Two concrete implementations are provided:
- [TCP spacepackets server](https://docs.rs/satrs/latest/satrs/hal/std/tcp_server/struct.TcpSpacepacketsServer.html)
to parse tightly packed CCSDS Spacepackets.

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@ -1,13 +1,14 @@
# Framework Design
# Library Design
Satellites and space systems in general are complex systems with a wide range of requirements for
both the hardware and the software. Consequently, the general design of the framework is centered
both the hardware and the software. Consequently, the general design of the library is centered
around many light-weight components which try to impose as few restrictions as possible on how to
solve certain problems.
solve certain problems. This is also the reason why sat-rs is explicitely called a library
instead of a framework.
There are still a lot of common patterns and architectures across these systems where guidance
of how to solve a problem and a common structure would still be extremely useful to avoid pitfalls
which were already solved and to avoid boilerplate code. This framework tries to provide this
which were already solved and to avoid boilerplate code. This library tries to provide this
structure and guidance the following way:
1. Providing this book which explains the architecture and design patterns in respect to common
@ -18,7 +19,7 @@ structure and guidance the following way:
3. Providing a good test suite. This includes both unittests and integration tests. The integration
tests can also serve as smaller usage examples than the large `satrs-example` application.
This framework has special support for standards used in the space industry. This especially
This library has special support for standards used in the space industry. This especially
includes standards provided by Consultative Committee for Space Data Systems (CCSDS) and European
Cooperation for Space Standardization (ECSS). It does not enforce using any of those standards,
but it is always recommended to use some sort of standard for interoperability.
@ -30,10 +31,10 @@ Flying Laptop Project by the University of Stuttgart with Airbus Defence and Spa
It has flight heritage through the 2 mssions [FLP](https://www.irs.uni-stuttgart.de/en/research/satellitetechnology-and-instruments/smallsatelliteprogram/flying-laptop/)
and [EIVE](https://www.irs.uni-stuttgart.de/en/research/satellitetechnology-and-instruments/smallsatelliteprogram/EIVE/).
Therefore, a lot of the design concepts were ported more or less unchanged to the `sat-rs`
framework.
library.
FLP is a medium-size small satellite with a higher budget and longer development time than EIVE,
which allowed to build a highly reliable system while EIVE is a smaller 6U+ cubesat which had a
shorter development cycle and was built using cheaper COTS components. This framework also tries
shorter development cycle and was built using cheaper COTS components. This library also tries
to accumulate the knowledge of developing the OBSW and operating the satellite for both these
different systems and provide a solution for a wider range of small satellite systems.

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@ -1,6 +1,6 @@
# sat-rs Example Application
The `sat-rs` framework includes a monolithic example application which can be found inside
The `sat-rs` library includes a monolithic example application which can be found inside
the [`satrs-example`](https://egit.irs.uni-stuttgart.de/rust/sat-rs/src/branch/main/satrs-example)
subdirectory of the repository. The primary purpose of this example application is to show how
the various components of the sat-rs framework could be used as part of a larger on-board

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The sat-rs book
======
This book is the primary information resource for the [sat-rs framework](https://egit.irs.uni-stuttgart.de/rust/sat-rs)
This book is the primary information resource for the [sat-rs library](https://egit.irs.uni-stuttgart.de/rust/sat-rs)
in addition to the regular API documentation. It contains the following resources:
1. Architecture informations and consideration which would exceeds the scope of the regular API.
@ -12,10 +12,15 @@ in addition to the regular API documentation. It contains the following resource
# Introduction
The primary goal of the sat-rs framework is to provide re-usable components
The primary goal of the sat-rs library is to provide re-usable components
to write on-board software for remote systems like rovers or satellites. It is specifically written
for the special requirements for these systems.
It should be noted that sat-rs is early-stage software. Important features are missing. New releases
with breaking changes are released regularly, with all changes documented inside respective
changelog files. You should only use this library if your are willing to work in this
environment.
A lot of the architecture and general design considerations are based on the
[FSFW](https://egit.irs.uni-stuttgart.de/fsfw/fsfw) C++ framework which has flight heritage
through the 2 missions [FLP](https://www.irs.uni-stuttgart.de/en/research/satellitetechnology-and-instruments/smallsatelliteprogram/flying-laptop/)