Aerospace Instrument-Making Annotation << Back Synergetic synthesis of basic vector control laws for solid-state space orientation systems AL.A. Kolesnikov The problem of the vectorial control laws synthesizing of the spatial orientation of space flight vehicles in initial non-linear statement is esteemed. The indicated problem is decided on the basis of methods of the synergetic theory of control. In an analytic form the base control laws guaranteeing an asymptotic stability of motion in whole and the desirable quality of the spacecraft orientation processes are obtained.