Editing Instrumentation (section)

===Aircraft===
Early aircraft had a few sensors.<ref>[http://www.cap-ny153.org/aircraftinstrumentation.htm Aircraft Instrumentation – Leroy R. Grumman Cadet Squadron<!-- Bot generated title -->]</ref> "Steam gauges" converted air pressures into needle deflections that could be interpreted as altitude and airspeed. A magnetic compass provided a sense of direction. The displays to the pilot were as critical as the measurements.

A modern aircraft has a far more sophisticated suite of sensors and displays, which are embedded into [[avionics]] systems. The aircraft may contain [[inertial navigation system]]s, [[global positioning system]]s, [[weather radar]], autopilots, and aircraft stabilization systems. Redundant sensors are used for reliability. A subset of the information may be transferred to a [[Event data recorder|crash recorder]] to aid mishap investigations. Modern pilot displays now include computer displays including [[head-up display]]s.

[[Air traffic control radar beacon system|Air traffic control radar]] is a distributed instrumentation system. The ground part sends an electromagnetic pulse and receives an echo (at least). Aircraft carry transponders that transmit codes on reception of the pulse. The system displays an aircraft map location, an identifier and optionally altitude. The map location is based on sensed antenna direction and sensed time delay. The other information is embedded in the transponder transmission.