Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
- Авторы: Nikitin A.V.1, Soldatkin V.V.1, Soldatkin V.M.1
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Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 59, № 4 (2016)
- Страницы: 587-594
- Раздел: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journals.rcsi.science/1068-7998/article/view/229927
- DOI: https://doi.org/10.3103/S1068799816040231
- ID: 229927
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Аннотация
We consider the problem of measuring the altitude and speed parameters aboard a helicopter, as well as ways to improve the noise stability and accuracy of measuring at low and nearzero flight speeds at the expense of using the air flow data of the main rotor vortex column, the principles of complexation and filtering.
Об авторах
A. Nikitin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: w-soldatkin@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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