Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
- 作者: Nikitin A.V.1, Soldatkin V.V.1, Soldatkin V.M.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 59, 编号 4 (2016)
- 页面: 587-594
- 栏目: 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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详细
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.
作者简介
A. Nikitin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: w-soldatkin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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