Research of mission-control possibility software to information of inercial'nykh sensors of low class of exactness
The results of the modeling of joint work of the control system with the aircraft inertial navigation system are represented in this article .For improving the accuracy of the control the results of calibration of inertial sensors with are used. It is shown that the developed method of calibrati...
Збережено в:
Дата: | 2014 |
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Автор: | |
Формат: | Стаття |
Мова: | Russian |
Опубліковано: |
Journal of Mechanical Engineering
2014
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Теми: | |
Онлайн доступ: | https://journals.uran.ua/jme/article/view/19920 |
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Назва журналу: | Journal of Mechanical Engineering |
Репозитарії
Journal of Mechanical EngineeringРезюме: | The results of the modeling of joint work of the control system with the aircraft inertial navigation system are represented in this article .For improving the accuracy of the control the results of calibration of inertial sensors with are used. It is shown that the developed method of calibration of inertial sensors with middle accuracy allow to improve the quality of inertial measuring unit and use it in automatically control system of aircraft. |
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