Gravity-perturbed Earth Orbit Lambert Problem - OTB/fsolve
PDF document and MATLAB script that demonstrates how to solve the Earth orbit, J2-perturbed form of Lambert’s problem using fsolve from the MATLAB Optimization Toolbox. Lambert’s problem is concerned with the determination of an orbit that passes between two positions within a specified time-of-flight. This classic astrodynamic problem is also known as the orbital two-point boundary value problem (TPBVP) or the flyby and rendezvous problems.
Citation pour cette source
David Eagle (2024). Gravity-perturbed Earth Orbit Lambert Problem - OTB/fsolve (https://www.mathworks.com/matlabcentral/fileexchange/74213-gravity-perturbed-earth-orbit-lambert-problem-otb-fsolve), MATLAB Central File Exchange. Récupéré le .
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- Sciences > Physics > Gravitation, Cosmology & Astrophysics >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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Version | Publié le | Notes de version | |
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1.0.0 |