Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform


The paper deals with a method of determining and checking the angular deviation of the actual position of the optical astro-sighting device instrument (IO ASD) relative to its reference target position on a gyrostabilized platform (GSP). The structure of a three-degree-of-freedom gyrostabilizer (TGS) that makes it possible to solve the assigned problem is described. An algorithm of determining the angles of the actual position of the IO ASD on a GSP is presented. The results of verifying the method using the actual devices of the TGS are given.

About the authors

M. S. Degtyarev

Federal State Unitary Enterprise “Scientific & Production Association of Automatics named after Academician N.A. Semikhatov”

Author for correspondence.

Head of Unit

Russian Federation


  1. Ilyukhin I.M., Dikarev V.N. Optiko-elektronnye pribory uglovoy orientatsii kosmicheskikh letatel'nykh apparatov [Optical electric equipment of space vehicle angular attitude]. Moscow: Bauman Moscow State University Publ., 1999. 44 р.



Abstract: 2828

PDF (Russian): 1893




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