Shreyas Subramanian's repositories
flytsim-docker
Dockerization of FlytSIM, for easy deployment to linux, windows and mac
docker-alpine-sklearn
Alpine Python3 images with scikit-learn pre-installed
brogrammers-demo-site
:dragon: Product marketing template for Jekyll
awesome-github-badges
A curated list of awesome github README.md badges
DNGO-BO
Bayesian optimization with DNGO (Deep Networks for Global Optimization)
portfolio
portfolio on GoHugo.io
swig
swig docker image based on build-jessie image
EngineDiagnosticsTest001
Non working code
Turbofan-Engine-Model
Object-Oriented Turbofan Engine Model (.NET) Michael Olsen and Teddy Garland
FlapPyBird
A Flappy Bird Clone using python-pygame
neuroblox
Scratch style drag and drop Deep Learning model builder for Keras.
misc
Miscellaneous code for various purposes
GRUV
GRUV is a Python project for algorithmic music generation.
Aircraft6DoF
6 DoF aircraft simulator coded in MATLAB
XPlaneConnect
The X-Plane Communications Toolbox (XPC) is an open source research tool used to interact with the commercial flight simulator software X-Plane. XPC allows users to control aircraft and receive state information from aircraft simulated in X-Plane using functions written in C or MATLAB in real time over the network. This research tool has been used to visualize flight paths, test control algorithms, simulate an active airspace, or generate out-the-window visuals for in-house flight simulation software.
T-MATS
An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System, Numerical Methods, Newton-Raphson, Jacobian Calculation, Propulsion, Aircraft Engine, Jet, Turbofan, Turbojet, Compressor, Turbine, Nozzle, Inlet, open source
Formation-Flying
Formation Flying Repository
TTECTrA
An open source, semi-automated, control design tool for subsonic aircraft engine simulations written in the MATLAB/Simulink environment. The Tool for Turbine Engine Closed-loop Transient Analysis provides the user a preliminary estimate of the closed-loop transient performance of an engine model.
WellClear
Well-Clear Boundary Models for Integration of UAS in the NAS
OpenVSP
A parametric aircraft geometry tool