Updated 06 Dec 2019
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.
David Eagle (2021). 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. Retrieved .
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