On the solution of the optimal control synthesis problem of spacecraft reorientation in sensing hardware redirection by one successive approximations method

The optimal control problem of spacecraft orientation in sensing hardware redirection at paths transition intervals is considered. To solve this problem the method of successive approximations is applied. Each approximation is connected with the decision support optimal control problems with functionals of the norm type in for control parameters vector. The support problems are solved using Krasovsky's maximum principle for vector norms with indicators .