Tuning for the Schuler Period of Primary Flight and Inertial Navigation Devices
DOI:
https://doi.org/10.52171/2076-0515_2023_15_02_07_14Keywords:
aircraft, attitude, pendulum, Schuler period, accelerometer, gyroscope, correctionAbstract
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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This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.