PDF document and four MATLAB scripts that demonstrate how to solve the Earth orbit, interplanetary, and J2-perturbed form of Lambert’s problem. 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.
David Eagle (2021). Lambert's Problem (https://www.mathworks.com/matlabcentral/fileexchange/39530-lambert-s-problem), MATLAB Central File Exchange. Retrieved .
This ephemeris algorithm is described in Chapter 31 of "Astronomical Algorithms" by Jean Meeus.
Hello, can you give some reference to the polynomial model used for the orbital elements as function of time in the "planet" function.
Youl find the algorithms for orb2eci algorithm and source code at the R.H Gooding paper
Can you give some references for the algorithm you have programmed in orb2eci file?
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