Navigation Grade Solid-State Wave Gyro for Air-Space Applications

Авторы: Perelyaev S.E., Bodunov S.B., Bodunov B.P.
Сборник: 2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)
Серия: Scopus
Год издания: 2022
Место издания: IEEE
Оригинальные версии: Волновой твердотельный гироскоп авиационно-космического применения навигационного класса точности
DOI: 10.23919/ICINS51784.2022.9815352
Аннотация: The applied aspects of fundamental theory of Van der Pol two degrees-of-freedom oscillator with external effective control are described [1]. Some issues of the feedback formation for effective control of the oscillations are considered. Research of new opportunities to improve accuracy parameters of solid-state integrating gyro in addition to known traditional techniques for new gyro errors reduction is suggested here. The applied aspects of the principal theory of the Van der Pol two degrees-of-freedom oscillator with external effective control based on the total energy of its oscillations and its implementation are presented. In the modern SSWG (promising inertial sensors of high accuracy) new design approaches–Force-to-Rebalance mode (FTR) and Whole Angle mode (integrating gyro) for various objects of air-space applications are presented.
Добавил в систему: Переляев Сергей Егорович

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