Nominal control program in problem of far rendezvous at geostationary orbit with low transversal thrust

The air of this research is obtaining of nominal control programs in problem of far rendezvous at geostationary orbit with low transversal thrust. The problem of control program designing in linear approximation divided to control in orbital plane and control in lateral direction. Motion in orbital plane is separate to secular and periodic. Using Pontriagins maximum principle, the structure of optimal control program with transversal thrust is determined. Base on optimal control program, the simple analytical control programs is obtained. Numeric simulation of rendezvous transfer with obtained control programs is carried out.