Spacecraft-Code / Vallado
https://celestrak.com/software/vallado-sw.asp
☆24Updated 7 years ago
Alternatives and similar repositories for Vallado:
Users that are interested in Vallado are comparing it to the libraries listed below
- ☆67Updated last month
- Conjunction Analysis and Screening with Python☆10Updated last year
- spacecraft orbit calculate☆55Updated 3 years ago
- Simulink model for Quaternion based Satellite Attitude dynamics and control☆10Updated 3 years ago
- LEOGPS - Satellite Navigation with GPS on Python!☆74Updated last year
- ☆25Updated 6 months ago
- A mirror of the Celestrak Vallado software astrodynamics software suite☆16Updated this week
- 🌎 sgp4 orbit propagation library for modern c++11☆25Updated this week
- A Python satellite guidance, navigation, and control library.☆33Updated this week
- Spacecraft Orbital Computations Kit (SpOCK)☆42Updated 2 months ago
- NOTE: This Tudat version is no longer supported. See https://docs.tudat.space/en/stable/ and https://github.com/tudat-team/tudat-bundle f…☆87Updated last year
- SpaceDSL is astrodynamics simulation library. This library can work on Windows, Linux and Mac OS.☆35Updated 4 years ago
- Simulates a satellite's Low Earth Orbit trajectory and additionally outputs it's Ground Track for a custom launch position and speed.☆57Updated 6 years ago
- Orbit Determination with Python☆119Updated last year
- Multi-Objective Low-Thrust Optimizer for Interplanetary Transfers☆32Updated 3 years ago
- Orbital Propagation Interface☆21Updated 3 years ago
- A simple orbit determination package (kalman filter estimation), which I coded for my master's thesis☆12Updated 3 years ago
- ATTIQUB - Attitude Control Simulation Engine (MATLAB), Unstable work in progress!☆12Updated 2 years ago
- Software for precise orbit determination of Low Earth Orbiters and gravity field recovery☆32Updated 4 months ago
- Relative Orbit Design and Visualisation in Python!☆13Updated 3 years ago
- ORBITM - Orbit maintenance, propulsion sizing, and life-time estimation of space objects!☆69Updated 9 months ago
- Determine the position, velocity, and orbit (in 3D) of satellite with given the initial vector (r0 &v0), using MATLAB☆11Updated last year
- ☆37Updated 4 years ago
- NASA Goddard's Evolutionary Mission Trajectory Generator (EMTG)☆55Updated 2 months ago
- ADCS simulations for the AcubeSAT nanosatellite☆13Updated 2 weeks ago
- A machine learning library for spacecraft collision avoidance☆55Updated last year
- A set of Lambert's problem solvers☆50Updated last month
- An attitude determination and control system simulator☆28Updated 6 years ago
- Applying extended Kalman filter to initial orbit determination.☆16Updated 4 years ago
- Python code to create an epheremides (a dataset of positions in orbit) for a mega-constellation of satellites in Low Earth Orbit.☆12Updated 3 years ago