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.
Analysis of Errors for Measuring Channels of Aircraft Air Data System with a Fixed Non-Protruding Flow Receiver
Russian Aeronautics ; 60 , 4 ; 481-487
2017-10-01
7 pages
Article (Journal)
Electronic Resource
English
System for Measuring Satellite Navigation System Receiver Errors
Online Contents | 2005
|