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Method of controllung the angular position of IO ASD relative to the system of coordinates of a gyrostabilized platform
- Authors: Degtyarev M.S.1
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Affiliations:
- Federal State Unitary Enterprise “Scientific & Production Association of Automatics named after Academician N.A. Semikhatov”
- Issue: Vol 13, No 1 (2014)
- Pages: 189-193
- Section: ELECTRONICS, MEASURING EQUIPMENT, RADIO ENGINEERING AND COMMUNICATION
- URL: https://journals.ssau.ru/vestnik/article/view/1712
- DOI: https://doi.org/10.18287/1998-6629-2014-0-1(43)-189-193
- ID: 1712
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Abstract
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.
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About the authors
M. S. Degtyarev
Federal State Unitary Enterprise “Scientific & Production Association of Automatics named after Academician N.A. Semikhatov”
Author for correspondence.
Email: degtermisha@mail.ru
Head of Unit
Russian FederationReferences
- 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.
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