Aerospace Instrument-Making Annotation << Back Stability and limiting cycles of system of stabilization of the satellite with an elastic rod and gas jet engines with the constant time of delay K.P. Andreychenko, D.K. Andreychenko The system of the differential equations of the satellite perturbed by the moment of outside force of driving with an elastic rod is composed. On the basis of the exact decision of the linearized equations set of the transfer function of system of stabilization in the form of the fraction is obtained, the numerator and which denominator are quazipolynomials. In space of coefficients of feedbacks areas of stability are constructed in view of time of delay in gas jet actuating engines, transitive functions of an error of stabilization are analysed. Limiting cycles are explored and the behavior of the satellite is analysed at loss of stability