Circular Restricted 3-Body Problem - Orbital Toolbox

バージョン 1.0.0 (29.2 KB) 作成者: Luigi De Maria
Collection of codes to simulate the CR3BP.
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更新 2022/9/3

ライセンスの表示

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.

引用

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. 取得済み .

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作成: R2022a
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