Planar Bicircular Restricted 4-Body Problem (PBR4BP)
Version 1.0.0 (3.53 KB) by
Luigi De Maria
Collection of codes to propagate orbits in the Planar Bicircular Restricted 4-Body Problem.
The codes collected here are meant to propagate and present the orbit of a spacecraft/particle in the Earth-Moon-Sun Planar Bicircular Restricted 4-Body Problem. The masses are organised as follows:
- Primary = Earth
- Secondary = Moon
- Tertiary = Sun
- Quaternary = Spacecraft
The codes allora to:
- PBR4BP_data.m = Produces the parameters used in the PBR4BP
- PBR4BP.m = Propagator in this astrodynamical model
- Syn2ECI = Transformation from PBR4BP Synodic r.f. (rotating frame) to Earth Centred Inertial r.f. (ECI), both in dimensionless forms.
- Syn2MCI = Transformation from PBR4BP Synodic r.f. (rotating frame) to Moon Centred Inertial r.f. (MCI), both in dimensionless forms.
Cite As
Luigi De Maria (2024). Planar Bicircular Restricted 4-Body Problem (PBR4BP) (https://www.mathworks.com/matlabcentral/fileexchange/119373-planar-bicircular-restricted-4-body-problem-pbr4bp), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2021a
Compatible with any release
Platform Compatibility
Windows macOS LinuxTags
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!Discover Live Editor
Create scripts with code, output, and formatted text in a single executable document.
Version | Published | Release Notes | |
---|---|---|---|
1.0.0 |