Aerospace Instrument-Making Annotation << Back The analysis and synthesis of the controlled gyrostabilizer with the variable bearing constitutive corner of aircraft V.I. Rodionov Examination of the analysis methodology of the dynamics of the biaxial controlled gyrostabilizer, working in the guiding system of the device sighting line onboard the aircraft with variable bearing constitutive corner, calling the aircraft swinging and angular motion of the device sighting line. Synthesis of the controllers in stabilization circuits carried out.