Email this article Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
- Authors: Nikitin A.V.1, Soldatkin V.V.1, Soldatkin V.M.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 587-594
- Section: 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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Abstract
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.
About the authors
A. V. Nikitin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. V. Soldatkin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: w-soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. M. Soldatkin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
