Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices

Authors

  • Karimli T.I. Azerbaijan National Academy of Aviation (Mardakan ave. 30, Baku, AZ1045, Azerbaijan)

DOI:

https://doi.org/10.52171/2076-0515_2023_15_02_07_14

Keywords:

aircraft, attitude, pendulum, Schuler period, accelerometer, gyroscope, correction

Abstract

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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Published

2023-06-30

How to Cite

T.I., K. (2023). Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices. Herald of Azerbaijan Engineering Academy, 15(2), 7–14. https://doi.org/10.52171/2076-0515_2023_15_02_07_14

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