A MATLAB Function for Computing Gravity in the Modified Equinoctial Coordinate System
版本 1.0.0.0 (2.1 KB) 作者:
David Eagle
Computes gravity due to the first four zonal harmonics in the modified equinoctial coordinate system
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.
引用格式
David Eagle (2024). 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. 检索来源 .
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R2012b
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- Aerospace and Defense > Aerospace Toolbox > Standard Workflow Procedures > Coordinate Systems >
- Aerospace and Defense > Aerospace Toolbox > Environmental Models >
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1.0.0.0 |