Browse Topic: Vehicle front ends

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This SAE Aerospace Standard (AS) covers air data computer equipment (hereinafter designated the computer) which when connected to sources of aircraft electrical power, static pressure, total pressure, outside air temperature, and others specified by the manufacturer (singly or in combination) provides some or all of the following computed air data output signals (in analog and/or digital form) which may supply primary and/or standby flight instruments: Pressure Altitude Pressure Altitude, Baro-Corrected Vertical Speed Calibrated Airspeed Mach Number Maximum Allowable Airspeed Over-speed Warning Total Air Temperature
A-4 Air Data Subcommittee
If you have considerable experience from industry and government in developing complex systems, one thing nice about being a Professor at a leading technical university is being able to help implement improvements in the education and development of complex systems, especially Vertical Lift Aircraft (VLA) systems. This is particularly true if you have the opportunity to participate as a member of major national efforts to implement improvements; as well as if you have the opportunity to serve on independent "red teams" reviewing industry proposals for complex system development. Fortunately, I have had these opportunities in my 35 years as the rotorcraft design professor in the School of Aerospace Engineering, Georgia Tech and as the Director for the Georgia Tech national Vertical Lift Research Center of Excellence (VLRCOE) for the past 33 years. The particular area I have pursued is development and implementation of an Integrated Product and Process Development (IPPD) methodology that
Schrage, DanielPatel, Srujal
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