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Development of the measuring complex with reduced regulator
Author(s) -
Guolai Yang,
Danhe Chen,
M. S. Selezneva,
K. A. Neusypin
Publication year - 2019
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1311/1/012037
Subject(s) - regulator , inertial navigation system , nonlinear system , control theory (sociology) , representation (politics) , computer science , navigation system , inertial frame of reference , control engineering , engineering , artificial intelligence , control (management) , physics , chemistry , quantum mechanics , politics , political science , law , biochemistry , gene
In this paper the measuring complex of a prospective aircraft is investigated. The accuracy of navigation definitions is improved by compensating for errors in the inertial navigation system structure. In this paper based on a reduced nonlinear regulator performed the correction of navigation information, and the state dependent coefficient (SDC) representation of the nonlinear model of inertial navigation system errors is used to obtain the regulator.

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