This 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 for one or two possible interplanetary injection opportunities. This information can be used as initial guesses for other trajectory simulations.
David Eagle (2020). Impulsive Hyperbolic Injection from a Circular Earth Park Orbit (https://www.mathworks.com/matlabcentral/fileexchange/38963-impulsive-hyperbolic-injection-from-a-circular-earth-park-orbit), MATLAB Central File Exchange. Retrieved .
Clarification updates to the MATLAB script and PDF user's guide.