On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data
DOI:
https://doi.org/10.31713/MCIT.2023.009Ключові слова:
inertial navigation system, accelerometer, gyroscope, orientation angles, aerial vehicle, trajectoryАнотація
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.
Посилання
Завантаження
Опубліковано
2023-11-22
Номер
Розділ
Mathematical, computer modeling and computational methods
Як цитувати
On the problems of determining the trajectory of an aerial vehicle based on inertial navigation system data. (2023). Моделювання, керування та інформаційні технології, 6, 38-41. https://doi.org/10.31713/MCIT.2023.009
