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A MATLAB Function for Computing Gravity in the Modified Equinoctial Coordinate System

version (2.09 KB) by David Eagle
Computes gravity due to the first four zonal harmonics in the modified equinoctial coordinate system


Updated 15 Feb 2015

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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.

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MATLAB Release Compatibility
Created with R2012b
Compatible with any release
Platform Compatibility
Windows macOS Linux