Circular Restricted 3-Body Problem - Orbital Toolbox

Version 1.0.0 (29,2 ko) par Luigi De Maria
Collection of codes to simulate the CR3BP.
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Mise à jour 3 sept. 2022

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Here is a small collection of functions developed to simulate the CR3BP.
It includes:
  • build_R_Syn2RTN: build rotation matrix from Synodic r.f. to RTN r.f.
  • cr3bpCplus_mex: propagator developed using Matlab Coder (higher computational efficincy)
  • CR3BPunpert: standard propagator using state-space system
  • dynamicsSTM_CR3BP: construction of State Matrix
  • stateTransCR3BP: propagation of State Transition Matrix
  • Syn2ECI: tranform Synodic state into ECI state
  • ECI2Syn: transform ECI state into Synodic state
For each function everything is deeply explained in the header. Just remember that propagators shall be used with ODE solvers calling them as handle-functions.

Citation pour cette source

Luigi De Maria (2024). Circular Restricted 3-Body Problem - Orbital Toolbox (https://www.mathworks.com/matlabcentral/fileexchange/117115-circular-restricted-3-body-problem-orbital-toolbox), MATLAB Central File Exchange. Récupéré le .

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Créé avec R2022a
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Version Publié le Notes de version
1.0.0