Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices
DOI:
https://doi.org/10.52171/2076-0515_2023_15_02_07_14Ключевые слова:
aircraft, attitude, pendulum, Schuler period, accelerometer, gyroscope, correctionАннотация
The article gives a review of operation of devices for measuring the spatial position of static and dynamic objects. Mechanical pendulums for determining the spatial position of an acceleratedly moving object with a disrturbed action and a classical solution for eliminating the perturbing inertial disrturbanse are considered. Variants of an universal-purpose pendulum undisrturbed under the disrturbanse of inertia force are presented, in which there is no need to adjust for the Schuler period.
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Опубликован
2023-06-30
Как цитировать
T.I., K. (2023). Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices. Вестник Азербайджанской инженерной академии, 15(2), 7–14. https://doi.org/10.52171/2076-0515_2023_15_02_07_14
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Articles
Лицензия
Это произведение доступно по лицензии Creative Commons «Attribution-NonCommercial» («Атрибуция — Некоммерческое использование») 4.0 Всемирная.
