Email this article Analysis of Errors for Measuring Channels of Aircraft Air Data System with a Fixed Non-Protruding Flow Receiver
- Authors: Krylov D.L.1, Soldatkin V.M.2, Efremova E.S.2
-
Affiliations:
- AO Aeropribor Voskhod
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 4 (2017)
- Pages: 481-487
- Section: Aircraft Equipment
- URL: https://journal-vniispk.ru/1068-7998/article/view/230255
- DOI: https://doi.org/10.3103/S1068799817040018
- ID: 230255
Cite item
Open Access
Access granted
Subscription Access
Abstract
A functional diagram and algorithms of processing the measuring channels of aircraft air data system with a fixed non-protruding flow receiver are considered. The technique and analysis of methodical and instrument errors in measuring the altitude-speed parameters of aircraft in the system channels are presented.
About the authors
D. L. Krylov
AO Aeropribor Voskhod
Email: w_soldatkin@mail.ru
Russian Federation, ul. Goncharnya 20/1, Moscow, 109240
V. M. Soldatkin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: w_soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111.
E. S. Efremova
Tupolev Kazan National Research Technical University
Email: w_soldatkin@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111.
Supplementary files
