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.
引用格式
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. 检索来源 .
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