Impulsive Hyperbolic Injection from an Earth Orbit - OTB
The hyper2_matlab.m MATLAB script determines the orbital elements and state vectors of the park orbit and departure hyperbola at injection, and the injection delta-v vector and magnitude. This information can be used as initial guesses for other trajectory simulations. This script uses the MATLAB Optimization Toolbox to find the optimal coplanar or non-coplanar transfer maneuver.
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David Eagle (2024). Impulsive Hyperbolic Injection from an Earth Orbit - OTB (https://www.mathworks.com/matlabcentral/fileexchange/73588-impulsive-hyperbolic-injection-from-an-earth-orbit-otb), MATLAB Central File Exchange. Recuperado .
Compatibilidad con la versión de MATLAB
Compatibilidad con las plataformas
Windows macOS LinuxCategorías
- Aerospace > Aerospace Blockset > Visualization >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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Versión | Publicado | Notas de la versión | |
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1.0.0 |