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ADC (3)
Usado para
air data computer
Definição1
An aircraft computer that receives and processes pitot pressure, static pressure, and temperature to calculate very precise altitude, indicated airspeed, true airspeed, and air temperature.
Fonte1
FEDERAL AVIATION ADMINISTRATION. Pilot's handbook of aeronautical knowledge. [s.l.], 2008. Disponível em: http://www.faa.gov/regulations_policies/handbooks_manuals/av iation/pilot_handbook/media/PHAK%20-%20Cover-Preface.pdf. Acesso em: 26 jun. 2014.
Definição2
ADC calculates flight parameters such as true air speed (TAS) and static pressure from air date sensors such as pilot head, total temperature probes and angle of attack sensor; drives displays and indicators (e.g. altitude, IAS), sets gains in automatic pilot, and gives information to other aircraft systems.
Fonte2
MULTILINGUAL aeronautical dictionary, or, dictionary aeronautique multilingue: english, french, spanish, dutch, greek, italian,portuguese, turkish. London: Technical Editing and reproduction Ltd, 1980.
Definição3
An electronic digital computer in aircraft that senses or computes static and pilot pressure, outside air and total air temperature, IAS (indicated air speed), TAS (true air speed), pressure altitude, Mach number, angle of attack, and angle of yaw. All these are corrected for their known errors. Engine and flight control system computers use the output of air data computers.
Fonte3
KUMAR, Bharat (ed.). An illustrated dictionary of aviation. New York: McGraw-Hill, c2005. 752 p.
Fonte4
EMBRAER. Technical dictionary english-portuguese. [São José dos Campos], 2001.
Português
computador de dados aerodinâmicos