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Add .gitignore, license and readme
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aryadas98 committed Jun 9, 2018
1 parent 4e7fc3b commit b494c61
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5 changes: 5 additions & 0 deletions AUTHORS.rst
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==========
Developers
==========

* Arya Das <[email protected]>
21 changes: 21 additions & 0 deletions LICENSE
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MIT License

Copyright (c) 2017 AerospaceResearch

Permission is hereby granted, free of charge, to any person obtaining a copy
of this software and associated documentation files (the "Software"), to deal
in the Software without restriction, including without limitation the rights
to use, copy, modify, merge, publish, distribute, sublicense, and/or sell
copies of the Software, and to permit persons to whom the Software is
furnished to do so, subject to the following conditions:

The above copyright notice and this permission notice shall be included in all
copies or substantial portions of the Software.

THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR
IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE
AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER
LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM,
OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE
SOFTWARE.
7 changes: 7 additions & 0 deletions README.md
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# Orbitdeterminator-Webapp: A webapp for [Orbit Determinator](https://github.com/aerospaceresearch/orbitdeterminator)

## Quick Start

__orbitdeterminator__ is a package written in python3 for determining orbit of satellites based on positional data. Various filtering and determination algorithms are available for satellite operators to choose from.

See [here](http://orbit-determinator.readthedocs.io/en/latest/) for installation instructions and documentation.
6 changes: 2 additions & 4 deletions app.py
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import sys
import os.path

sys.path.append(os.path.abspath(os.path.join(os.path.dirname(__file__),os.path.pardir,'orbitdeterminator')))

from kep_determination.ellipse_fit import determine_kep
import orbitdeterminator.kep_determination.ellipse_fit as e_fit

app = dash.Dash()

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data = parse_file(file_content)
if (data.shape[0] > 0):
data_dict = [{'No.':'{:03d}'.format(i+1), 't':data[i][0], 'x':data[i][1], 'y':data[i][2], 'z':data[i][3]} for i in range(data.shape[0])]
kep, res = determine_kep(data[:,1:])
kep, res = e_fit.determine_kep(data[:,1:])

return [html.Div(children=file_name, className='section-titles'),

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1 change: 1 addition & 0 deletions requirements.txt
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Expand Up @@ -19,6 +19,7 @@ jupyter-core==4.4.0
kiwisolver==1.0.1
MarkupSafe==1.0
matplotlib==2.2.2
orbitdeterminator==1.0
nbformat==4.4.0
numpy==1.14.3
plotly==2.7.0
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