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

Автор(и)

DOI:

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

Ключові слова:

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

Анотація

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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Опубліковано

2023-11-22

Як цитувати

Sabziev, E. N., Hasanov, A., & Pashayev, A. (2023). On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data. Моделювання, керування та інформаційні технології, (6), 38–41. https://doi.org/10.31713/MCIT.2023.009

Номер

№ 6 (2023): Modeling, control and information technologies: Proceedings of VI International scientific and practical conference

Розділ

Mathematical, computer modeling and computational methods