Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
- Авторлар: Nikitin A.V.1, Soldatkin V.V.1, Soldatkin V.M.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 59, № 4 (2016)
- Беттер: 587-594
- Бөлім: 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
Дәйексөз келтіру
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.
Авторлар туралы
A. Nikitin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: w-soldatkin@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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