Skip to content

Latest commit

 

History

History
16 lines (12 loc) · 599 Bytes

README.md

File metadata and controls

16 lines (12 loc) · 599 Bytes

OrbitPropagator

This repository is a successor-fork of the Bachelor thesis on "Efficient trajectory modelling for space debris evolution" at TUM in collaboration with ESA.

It is part of the LADDS project and acts as the central engine for calculating the trajectory updates on all simulated particles.

Dependencies

  • C++17 Compiler
  • CMake (>= 3.10)

Build

build instructions for make:

mkdir build && cd build
cmake ..
make