The estimation error of the Runge-Kutta method in the task of reducing an angular momentum of a microsatellite

We consider the problem of numerical modeling of damping of a microsatellite with electromagnetic executive bodies. At the numerical integration of equations of motion of microsatellite used a seven-step Runge-Kutta method. The estimation error in the numerical integration of a equations of a motion through the application a seven-step and four-stage explicit Runge-Kutta methods is performed.