Research on High-Precision Measurement Systems of Modern Aircraft

Kai Shen; K. A. Neusypin; M. S. Selezneva; A. V. Proletarskii

doi:10.3103/S1068799818020186

Research on High-Precision Measurement Systems of Modern Aircraft

Kai Shen^*
, K. A. Neusypin
, M. S. Selezneva
, A. V. Proletarskii

^*Corresponding author for this work

Bauman Moscow State Technical University

Research output: Contribution to journal › Article › peer-review

3 Citations (Scopus)

Abstract

High-precision measurement systems of modern aircraft are studied in this paper. A measurement system with correction in the structure of inertial navigation system is introduced for highprecision aircraft. In the correction algorithms, a linear error model of the navigation system is usually used. With the aim of increasing the accuracy of the navigation system, we propose a nonlinear correction algorithm based on the state dependent coefficient representation of the nonlinear model.

Original language	English
Pages (from-to)	279-286
Number of pages	8
Journal	Russian Aeronautics
Volume	61
Issue number	2
DOIs	https://doi.org/10.3103/S1068799818020186
Publication status	Published - 1 Apr 2018
Externally published	Yes

Keywords

control algorithm
high-precision aircraft
inertial navigation system
measurement system
state dependent coefficient representation of nonlinear model

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10.3103/S1068799818020186

Cite this

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title = "Research on High-Precision Measurement Systems of Modern Aircraft",

abstract = "High-precision measurement systems of modern aircraft are studied in this paper. A measurement system with correction in the structure of inertial navigation system is introduced for highprecision aircraft. In the correction algorithms, a linear error model of the navigation system is usually used. With the aim of increasing the accuracy of the navigation system, we propose a nonlinear correction algorithm based on the state dependent coefficient representation of the nonlinear model.",

keywords = "control algorithm, high-precision aircraft, inertial navigation system, measurement system, state dependent coefficient representation of nonlinear model",

author = "Kai Shen and Neusypin, \{K. A.\} and Selezneva, \{M. S.\} and Proletarskii, \{A. V.\}",

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AU - Shen, Kai

AU - Neusypin, K. A.

AU - Selezneva, M. S.

AU - Proletarskii, A. V.

PY - 2018/4/1

Y1 - 2018/4/1

N2 - High-precision measurement systems of modern aircraft are studied in this paper. A measurement system with correction in the structure of inertial navigation system is introduced for highprecision aircraft. In the correction algorithms, a linear error model of the navigation system is usually used. With the aim of increasing the accuracy of the navigation system, we propose a nonlinear correction algorithm based on the state dependent coefficient representation of the nonlinear model.

AB - High-precision measurement systems of modern aircraft are studied in this paper. A measurement system with correction in the structure of inertial navigation system is introduced for highprecision aircraft. In the correction algorithms, a linear error model of the navigation system is usually used. With the aim of increasing the accuracy of the navigation system, we propose a nonlinear correction algorithm based on the state dependent coefficient representation of the nonlinear model.

KW - control algorithm

KW - high-precision aircraft

KW - inertial navigation system

KW - measurement system

KW - state dependent coefficient representation of nonlinear model

UR - https://www.scopus.com/pages/publications/85057088011

U2 - 10.3103/S1068799818020186

DO - 10.3103/S1068799818020186

M3 - Article

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ER -

Research on High-Precision Measurement Systems of Modern Aircraft

Abstract

Keywords

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