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Attitude ATTCS Automatic Take-off Thrust Control System AUPRTA Airplane Upset Prevention & Recovery Training Aid AVAIL Available Avionics: Aviation electronics AVSA "Adjust vertical speed adjust" TCAS Voice command to adjust traffic separation AWACS Airborne Warning and Control System: Airborne early warning and control (AEW&C) or Boeing E-3 ...
In conjunction with ARP4754, ARP4761 is used to demonstrate compliance with 14 CFR 25.1309 in the U.S. Federal Aviation Administration (FAA) airworthiness regulations for transport category aircraft, and also harmonized international airworthiness regulations such as European Aviation Safety Agency (EASA) CS–25.1309.
Download as PDF; Printable version; In other projects ... List of aviation, avionics, aerospace and aeronautical abbreviations ... List of government and military ...
An attitude and heading reference system (AHRS) consists of sensors on three axes that provide attitude information for aircraft, including roll, pitch, and yaw. These are sometimes referred to as MARG (Magnetic, Angular Rate, and Gravity) [ 1 ] sensors and consist of either solid-state or microelectromechanical systems (MEMS) gyroscopes ...
ATA 100 contains the reference to the ATA numbering system which is a common referencing standard for commercial aircraft documentation. This commonality permits greater ease of learning and understanding for pilots, aircraft maintenance technicians, and engineers alike.
The U.S. NASA Aviation Safety Program [2] [3] defines upset prevention and upset recovery as to prevent loss-of-control accidents due to aircraft upset after inadvertently entering an extreme or abnormal flight attitude. A Boeing-compiled list determined that 2,051 people died in 22 accidents in the years 1998–2007 due to LOC accidents. [1]
The acronym NOTAM came into common use following the ratification of the CICA, which came into effect on 4 April 1947, [citation needed] although early recorded use of the "Notice to Airmen" heading can be found in Flight International magazine in the UK. [11]
Attitude control – is controlling the orientation of an object with respect to an inertial frame of reference or another entity like the celestial sphere, certain fields, and nearby objects, etc. Controlling vehicle attitude requires sensors to measure vehicle orientation, actuators to apply the torques needed to re-orient the vehicle to a ...