Gyroscopic Flight Instruments are instruments which have a mechanical gyroscope incorporated into their design.
Description
Gyroscopic flight instruments of some description are used in most general aviation aircraft and in older commercial aircraft. Examples of such instruments include attitude indicators, heading indicators and turn coordinators (turn and slip indicator). The gyroscopes within the instruments are usually electrically or vacuum driven and make use of the basic gyroscopic principles to display the attitude of the aircraft. In more modern installations, mechanical gyroscopes have been replaced by laser gyros.
Gyroscopic Principles
The principal characteristic of a gyro which makes it suitable for use in attitude instruments is Rigidity in Space. A secondary gyroscopic principle which must be understood and compensated for, as necessary, is Precession. Explanation of the terms is as follows: