Many revolution low-thrust (MRLT) trajectory optimization with direct collocation using ICLOCS on MATLAB
Developed on MATLAB R2024a.
For initializing the repository, run
git clone --recurse-submodules https://github.com/Yuricst/DirectMRLT.git
git submodule update --init --recursive # if --recurse-submodules flag was forgotten
- ICLOCS: https://github.com/ImperialCollegeLondon/ICLOCS
- adigator: https://github.com/matt-weinstein/adigator
- Optimization : needed if using fmincon
- Signal Processing Toolbox : needed if using hp-grids (recommended)
- MEE dynamics
- Two-body
- Spherical harmonics
- SRP
- Eclipse path constraints