Abstract
Air data systems provide accurate information on quantities such as pressure altitude, vertical speed, calibrated airspeed, true airspeed, Mach number, static air temperature and air density ratio. This information is essential for the pilot to fly the aircraft safely and is also required by a number of key avionic subsystems which enable the pilot to carry out the mission. It is thus one of the key avionic systems in its own right and forms part of the essential core of avionic sub systems required in all modern aircraft, civil or military.
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Further reading
British Standard 2G199:1984, Tables relating altitudes airspeed and mach numbers for use in aeronautical instrument design and calibration.
Dommasch, D.D., Sherby, S.S., Connolly, T.F. Airplane aerodynamics: Pitman 1967
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© 2003 Springer Science+Business Media New York
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Collinson, R.P.G. (2003). Air Data and Air Data Systems. In: Introduction to Avionics Systems. Springer, Boston, MA. https://doi.org/10.1007/978-1-4419-7466-2_7
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DOI: https://doi.org/10.1007/978-1-4419-7466-2_7
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4757-5584-8
Online ISBN: 978-1-4419-7466-2
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