Fixed links

Author: jagoosw

README.md

@@ -8,7 +8,7 @@ CamPyRoS (Cambridge Python Rocketry Simulator) is a Python package which provide
 - Use of live wind data
 - Variable mass and moments of inertia models
 
-For a fuller documatation see the docs [here](https://cuspaceflight.github.io/CamPyRoS-Docs/)
+For a fuller documatation see the docs [here](https://campyros.readthedocs.io/)
 
 ## Getting started
 Currently not all dependancies are supported by the same install methods so the easiest install doesn't contain the full functionality. To install the core library:

docs/source/index.rst

@@ -22,7 +22,7 @@ Currently not all dependancies are supported by the same install methods so the
 
 The "wind" and "statistics" modules will not run. Statistics has a dependancy not fully supported by windows, to install it:
 
-`pip install ray` on most platforms, for Windows problems see [here](https://docs.ray.io/en/master/installation.html).
+`pip install ray` on most platforms, for Windows problems see `here <https://docs.ray.io/en/master/installation.html>`_.
 
 Wind depends on a library called iris which can only be installed with conda:
 
@@ -32,7 +32,7 @@ Wind depends on a library called iris which can only be installed with conda:
   conda install iris, iris_grib
 
 .. note::
-    Note: after some more testing this won't work for anyone on Windows, I am in the process fo sorting this out (the problem is a codec dependancy which there is no way for us to fix) by writing an library to read the other GFS distrobution method, see [gfspy](https://github.com/jagoosw/gfspy). You can still run and contribute without using the wind module. If you really want to use the wind module please [email]([email protected]) or message me and we can try and sort out access to something remote you can use to run it. 
+    Note: after some more testing this won't work for anyone on Windows, I am in the process fo sorting this out (the problem is a codec dependancy which there is no way for us to fix) by writing an library to read the other GFS distrobution method, see `getgfs <https://github.com/jagoosw/getgfs>`_. You can still run and contribute without using the wind module.
 
 This may then demand you install another library when you try to run it:
 
@@ -61,22 +61,22 @@ The repository contains some examples you can run:
 
 Helping out
 ===========
-If you would like to contribute please have a look at the [guidelines](CONTRIBUTING.md)
+If you would like to contribute please have a look at the `guidelines <https://github.com/cuspaceflight/CamPyRoS/blob/main/CONTRIBUTING.md>`_
 
 
 In progress
 ===========
 - **GUI:** An incomplete (and outdated) GUI has been made using Tkinter, and is in gui.py.
-- **Slosh modelling:** Some slosh modelling functions have been put together in slosh.py, based on the following source - [The Dynamic Behavior of Liquids in Moving Containers, with Applications to Space Vehicle Technology](https://ntrs.nasa.gov/citations/19670006555).
+- **Slosh modelling:** Some slosh modelling functions have been put together in slosh.py, based on the following source - `The Dynamic Behavior of Liquids in Moving Containers, with Applications to Space Vehicle Technology <https://ntrs.nasa.gov/citations/19670006555>`_.
 - **Wind variability:** Statistical analysis of historic wind forecasts and obervations are analysed to create a Guassian difference profile to vary the wind in the statistical models (see wind-stats branch for a very poorly documented insight to current progress)
 
 
 Potential for expansion
 =======================
 - **Multistage rockets**
-- **Fin cant, roll damping, and roll acceleration:** [OpenRocket Technical Documentation](http://openrocket.info/documentation.html)
-- **CFD coupling:** [PyFoam](https://openfoamwiki.net/index.php/Contrib/PyFoam), [Simulations of 6-DOF Motion with a Cartesian Method](https://pdfs.semanticscholar.org/ace3/5a61803390b0e0b70f6ca34492ad20a03e03.pdf)
-- **Multiphysics coupling:** [PRECICE](https://www.precice.org/)
+- **Fin cant, roll damping, and roll acceleration:** `OpenRocket Technical Documentation <http://openrocket.info/documentation.html>`_
+- **CFD coupling:** `PyFoam <https://openfoamwiki.net/index.php/Contrib/PyFoam>`_, `Simulations of 6-DOF Motion with a Cartesian Method <https://pdfs.semanticscholar.org/ace3/5a61803390b0e0b70f6ca34492ad20a03e03.pdf>`_
+- **Multiphysics coupling:** `PRECICE <https://www.precice.org/>`_
 
 Cite as
 =======
@@ -85,23 +85,23 @@ Daniel Gibbons, & Jago Strong-Wright. (2021, February 11). cuspaceflight/CamPyRo
 References
 ==========
 
-[1] - [Stochastic Six-Degree-of-Freedom Flight Simulator for Passively Controlled High-Power Rockets](https://ascelibrary.org/doi/10.1061/%28ASCE%29AS.1943-5525.0000051)
+[1] - `Stochastic Six-Degree-of-Freedom Flight Simulator for Passively Controlled High-Power Rockets <https://ascelibrary.org/doi/10.1061/%28ASCE%29AS.1943-5525.0000051>`_
 
-[2] - [Tangent ogive nose aerodynamic heating program: NQLD019](https://ntrs.nasa.gov/citations/19730063810)
+[2] - `Tangent ogive nose aerodynamic heating program: NQLD019 <https://ntrs.nasa.gov/citations/19730063810>`_
 
-[3] - [NASA Basic Considerations for Rocket Trajectory Simulation](https://apps.dtic.mil/sti/pdfs/AD0642855.pdf)
+[3] - `NASA Basic Considerations for Rocket Trajectory Simulation <https://apps.dtic.mil/sti/pdfs/AD0642855.pdf>`_
 
-[4] - [SIX DEGREE OF FREEDOM DIGITAL SIMULATION MODEL FOR UNGUIDED FIN-STABILIZED ROCKETS](https://apps.dtic.mil/dtic/tr/fulltext/u2/452106.pdf)
+[4] - `SIX DEGREE OF FREEDOM DIGITAL SIMULATION MODEL FOR UNGUIDED FIN-STABILIZED ROCKETS <https://apps.dtic.mil/dtic/tr/fulltext/u2/452106.pdf>`_
 
-[5] - [Trajectory Prediction for a Typical Fin Stabilized Artillery Rocket](https://journals.ekb.eg/article_23742_f19c1da1a61e78c1f5bb7ce58a7b30dd.pdf)
+[5] - `Trajectory Prediction for a Typical Fin Stabilized Artillery Rocket <https://journals.ekb.eg/article_23742_f19c1da1a61e78c1f5bb7ce58a7b30dd.pdf>`_
 
-[6] - [Central Limit Theorem and Sample Size](https://www.umass.edu/remp/Papers/Smith&Wells_NERA06.pdf)
+[6] - `Central Limit Theorem and Sample Size <https://www.umass.edu/remp/Papers/Smith&Wells_NERA06.pdf>`_
 
-[7] - [Monte Carlo Simulations: Number of Iterations and Accuracy](https://apps.dtic.mil/dtic/tr/fulltext/u2/a621501.pdf)
+[7] - `Monte Carlo Simulations: Number of Iterations and Accuracy <https://apps.dtic.mil/dtic/tr/fulltext/u2/a621501.pdf>`_
 
-[8] - [Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses](https://arc.aiaa.org/doi/abs/10.2514/3.62081)
+[8] - `Method for Calculating Aerodynamic Heating on Sounding Rocket Tangent Ogive Noses <https://arc.aiaa.org/doi/abs/10.2514/3.62081>`_
 
-[9] - [Six degree-of-freedom (6-DOF) Flight Simulation Check-cases](https://nescacademy.nasa.gov/flightsim/)
+[9] - `Six degree-of-freedom (6-DOF) Flight Simulation Check-cases <https://nescacademy.nasa.gov/flightsim/>`_