On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data

Authors

DOI:

https://doi.org/10.31713/MCIT.2023.009

Keywords:

inertial navigation system, accelerometer, gyroscope, orientation angles, aerial vehicle, trajectory

Abstract

Navigation in military UAVs requires the use of onboard inertial systems. An approach is proposed for noise filtering, refinement of initial and intermediate values when applying calculation algorithms based on the estimates of loads and angular velocity taken from sensors.

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Published

2023-11-22

Issue

No. 6 (2023): Modeling, control and information technologies

Section

Mathematical, computer modeling and computational methods

License

Copyright (c) 2023 Modeling, Control and Information Technologies: Proceedings of International scientific and practical conference

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

All materials are distributed under the terms of the Creative Commons Attribution 4.0 International License, which allows others to distribute the work with attribution to the authorship of this work and the first publication in this journal.

How to Cite

On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data. (2023). Modeling, Control and Information Technologies, 6, 38-41. https://doi.org/10.31713/MCIT.2023.009

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