Sequential Convex Programming Toolbox for nonconvex trajectory optimization.
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Updated
Aug 7, 2023 - Julia
Sequential Convex Programming Toolbox for nonconvex trajectory optimization.
Implementation of SCvx, linear MPC and LQR for trajectory generation and tracking
π°οΈ Satellite TLE tools in JavaScript: get lat/lon of satellites, get look angles, plot orbit lines, extract individual TLE elements, etc
Astrodynamics simulation framework
π π‘ π π‘ LEOGPS - Satellite Navigation with GPS on Python!
Spacecraft Simulation Environment Core codes
An Open Source Program that allows users to interact with a Spacecraft in a lab environment, pre-launch.
Open-source modeling and control toolkit for mobile-base robotic multibody systems
Spacecraft Orbital Computations Kit (SpOCK)
Opensat first generation cubesat bus, launch into orbit at 2016/11/11
Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.
Machine Learning + Spacecraft Trajectory Optimisation
Lossless convexification new results (mixed-integer problems)
Utility and framework for CCSDS/ECSS spacecraft and ground elements monitoring & control.
Spacecraft Pose Estimation: Robust 2D and 3D-Structural Losses and Unsupervised Domain Adaptation by Inter-Model Consensus
Study and implementations of different attitude estimation algorithms for spacecrafts.
ECSS Packet Utilization Standard implementation.
JSON files containing lots of interesting information on the people currently living in space for use in your project.
π π‘ π π‘ FORMFLYT - High fidelity orbit propagation for formation flying control in MATLAB!
On November 8, 2020, this project achieved the first use of deep convolutional neural networks (CNN) on-board a spacecraft.
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