Abstract The structural and functional scheme of helicopter air data system based on a stationary combined aerometric receiver using the aerometric field information of the main rotor vortex column is considered. According to the algorithms of information signal formation, the requirements to metrological characteristics of primary information sensors for the measurement channel system are substantiated.
Analysis of requirements to the measurement channels of helicopter air data system based on a stationary combined aerometric receiver
Russian Aeronautics (Iz VUZ) ; 54 , 1 ; 77-83
2011-03-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch