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

Elkhan Nariman Sabziev; Arif Hasanov; Adalat Pashayev

doi:10.31713/MCIT.2023.009

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

Authors

Elkhan Nariman Sabziev Institute of Control Systems https://orcid.org/0000-0001-8150-9439 (unauthenticated)
Dr. Arif Hasanov Military Scientific-Research Institute of National Defense University https://orcid.org/0000-0002-8814-1590 (unauthenticated)
Dr. Adalat Pashayev Institute of Control Systems https://orcid.org/0000-0001-9208-8430 (unauthenticated)

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: Proceedings of VI International scientific and practical conference

Section

Mathematical, computer modeling and computational methods

How to Cite

On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data. (2023). MCIT: Proceedings of International Scientific and Practical Conference, 6, 38-41. https://doi.org/10.31713/MCIT.2023.009

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

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