Instrument that measures the aircraft's speed in nautical miles per hour
Attitude indicator
Instrument that displays the aircraft's attitude relative to the earth's horizon
Altimeter
Instrument that shows the barometric altitude as measured in feet
Heading indicator
Instrument that indicates the direction in which the aircraft is flying
Turn coordinator
Instrument that displays the rate of turn in the roll axis and the amount of bank in the yaw axis
Vertical speed indicator
Instrument that provides information about the rate of ascent and descent in feet per minute
Electronic attitude directional indicator
In a glass cockpit, the artificial horizon with lateral bars superimposed, displaying computer-generated pitch and bank steering commands from the Flight Director computer
Horizon situational indicator
Digital instrument that is a combination of navigation commands from VOR or GPS receivers for en-route guidance and from the ILS for terminal guidance
Engine indication crew alerting system
System manufactured by Boeing aircraft that performs the monitoring of aircraft systems, with the upper displaying engine performance data and the lower is known as Multifunction Display
Binary numbering system
Numbering system used in computer architecture and digital electronics, with a base 2 and a series of 0s and 1s forming strings known as machine language
DeMorgan's theorem
Theorem that states that two separate terms NAND together are the same as the two terms inverted and OR
Ex NOR
Logic gate that produces a Logic 0 output whenever either one of the two inputs is at Logic 1 and the other is at Logic 0
Boolean algebra
Frequently used to describe logical operations in avionics systems and analyze digital circuits
Exclusive-OR gate
When either of the inputs is Logic 1, but not both, the output is Logic 1
NAND gate
Combination of a NOT gate and an AND gate
OR gate
To have an output of Logic 1, at least one input must be at Logic 1
Inverter/NOT gate
If the input is logic 1, the output is logic 0
Buffer gate
Type of gate that has the same output as the input and does not affect the logical state of a digital signal
NOR gate
Combination of an OR gate and an inverter
Computers found on board aircraft are used to provide vehicle and utility control; flight management; navigation, communication, and verification; caution and warning; and other essential functions
Main Memory
Stores information for later erasure by the CPU
Control Bus
Provides control signals between the CPU, Main Memory, and the I/O system in a parallel bus
Flash memory
Faster than EEPROM, allows memory to be rewritten and reprogrammed into blocks of memory
System software
Designed to directly operate computer hardware
Binary
Computer process information using digital data that is coded in single decimal digits, known as 'bits'
Data Transfer System (DTS)
External secondary data storage device used for downloading navigation flight plans to the FMC and for downloading maintenance data
Input and Output (I/O) system
Converts the information to other forms to facilitate communication with other onboard computers and their operators through external unidirectional serial buses
PROM
Ordinary PROM cannot be changed once assembled
Aircraft computer systems must be certified to be fail-safe, allowing hard or software errors cannot cause a catastrophic safe-of-flight incident
ADC
Converts a sequence of binary digits into 'impulses' that are then processed by a deconstruction filter to smooth out the step response into continuous curves
Ethernet was first introduced in 1970 - 1980
IEEE 1394 (Firewire)
Originally developed by the IEEE for the consumer electronics industry as a parallel point-to-point interface
Time-Division Multiplexing
Enables different forms of information to be received through one communication system
Digital signals have only two levels of voltage; high ON and low for OFF
Microprocessor
Retrieves and processes instructions and coordinates the flow of data throughout the computer
Integer Arithmetic Logic Unit
Designed to carry out operations typically addition, subtraction, multiplication, division, square root, and bit shifting
Motorola MC68000
Microprocessor used in the Boeing 777, running at clock speeds of 20 Mhz
Address Latch Enable
Function of a microprocessor that indicates which bytes on the address bus are valid to use
CMOS (Complementary-Metal Oxide Semiconductor)
Used for the voltage and ground for the microprocessor, 3.3 volts DC
Medium Scale Integration
Used for adders, counters, registers, comparators, encoders, decoders, multiplexers, de-multiplexers, etc.