Mathematical Model of Gyroscope with Contactless Suspended Rotor and Three-component Accelerometer for Solving Problems of Autonomous Autonomous Navigation

The problem of creating a mathematical model of a free three-degree gyroscope with a contactless suspended rotor and a three-component accelerometer for solving problems of high-precision autonomous navigation is solved. The problem under consideration includes determination of kinematic relations of the gyro device and solution of a direct problem for finding navigation parameters for a stationary base. The suspension system of these gyroscopes is practically indifferent to the environment in which the gyro operates, but in order to reduce braking moments, the gyro rotor is placed in a vacuum chamber. The given structure of vector relationships between coordinate systems and model parameters allows us to write down several groups of equations regarding the angular positions of the gyro rotor and its angular velocities.

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Publication Details

Journal
Electronics and Control Systems
Published
2025-06-30
DOI
https://doi.org/10.18372/1990-5548.84.20201
Primary Topic
Advanced Data Processing Techniques
Type
article
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article

Mathematical Model of Gyroscope with Contactless Suspended Rotor and Three-component Accelerometer for Solving Problems of Autonomous Autonomous Navigation

Yuriy Kemenyash, Oleg Smirnov
Electronics and Control Systems
Advanced Data Processing Techniques
article

Mathematical Model of Gyroscope with Contactless Suspended Rotor and Three-component Accelerometer for Solving Problems of Autonomous Autonomous Navigation

Yuriy Kemenyash, Oleg Smirnov
article en

Abstract

The problem of creating a mathematical model of a free three-degree gyroscope with a contactless suspended rotor and a three-component accelerometer for solving problems of high-precision autonomous navigation is solved. The problem under consideration includes determination of kinematic relations of the gyro device and solution of a direct problem for finding navigation parameters for a stationary base. The suspension system of these gyroscopes is practically indifferent to the environment in which the gyro operates, but in order to reduce braking moments, the gyro rotor is placed in a vacuum chamber. The given structure of vector relationships between coordinate systems and model parameters allows us to write down several groups of equations regarding the angular positions of the gyro rotor and its angular velocities.

Electronics and Control SystemsVol. 2(84)
National University "Kyiv Aviation Institute" (UA)
Openalex Percentile: Top 79%
Advanced Data Processing Techniques
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