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today we will talk about the attitude and heading reference system which like the air data computer has helped the transition from the conventional analog instruments to the new digital systems however before going into detail with this system we must see how conventional analog instruments work in the case of gyroscopic instruments each one has its own gyroscope specifically designed to measure a certain parameter this means that each instrument has its own gyro gimbals gears and other moving parts this results in more complex isolated systems with errors and inaccuracies due to mechanical imperfections friction gyroscopic drift among others and in addition to this in the case of the heading indicator the crew must manually correct the indication using the magnetic compass as a reference and to do so the aircraft must be flying in straight flight with a constant speed as these are the only conditions under which the compass gives a correct heading indication all this results in higher
