Given an input orbital state in the modified equinoctial coordinate system, this MATLAB function computes the acceleration due to Earth gravity (unnormalized J2, J3 and J4) in this same coordinate system.
David Eagle (2021). A MATLAB Function for Computing Gravity in the Modified Equinoctial Coordinate System (https://www.mathworks.com/matlabcentral/fileexchange/49713-a-matlab-function-for-computing-gravity-in-the-modified-equinoctial-coordinate-system), MATLAB Central File Exchange. Retrieved .
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