Cowell's Method for Earth Satellites
PDF document and an interactive MATLAB script named cowell.m that predicts the long-term behavior of an Earth satellite subject to perturbations. This script implements a special perturbation solution of orbital motion using a variable step size Runge-Kutta-Fehlberg (RKF78) integration method to numerically solve Cowell’s form of the system of differential equation subject to the central body gravity and other external forces. This is also called the orbital initial value problem (IVP).
引用格式
David Eagle (2024). Cowell's Method for Earth Satellites (https://www.mathworks.com/matlabcentral/fileexchange/39703-cowell-s-method-for-earth-satellites), MATLAB Central File Exchange. 检索来源 .
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- Industries > Aerospace and Defense > CubeSat and Satellites >
- Aerospace and Defense > Aerospace Blockset > Reference Applications >
- Sciences > Geoscience > Earth and Planetary Science >
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