Category
page 1Fault tolerance
uninterruptible power supply
electrical device that uses batteries to prevent a power flow interruption

fly-by-wire
thumb|The Airbus A320 family was the first [[airliner to feature a full glass cockpit and digital fly-by-wire flight control system. The only analogue instruments were the radio magnetic indicator, brake pressure indicator, standby altimeter and artificial horizon, the latter two being replaced by a digital integrated standby instrument system in later production models.]]
Fly-by-wire (FBW) is a system that replaces the conventional manual flight controls of an aircraft with an electronic interface. The movements of flight controls are converted to electronic signals, and flight control comput
amplitude-shift keying
Type of Data Encoding
fault tolerance
ability of a system to continue functioning despite erroneous inputs or faults within some of its components
fault
abnormal condition or defect at the component, equipment, or sub-system level which may lead to an equipment failure
emergency power system
independent backup source of electrical power that supports important electrical systems on loss of normal power supply
collateral circulation
alternate blood flow around a blockage