About orientation'S control of shutters of solar batteries of spacecraft

In this paper consider the problem of the control of the motions of solar panels of spacecraft in a circular orbit. It is modeled by mechanical system with three degrees of freedom. Two types of active control on the principle of feedback, which realize asymptotically stable of given non-stationary program motions of batteries, are constructed. The solution of the problem is given on the basis of the first method of the classical stability theory.