These sensors are involved in the detection of motion in a universal referenced set.
inertial sensors
most commonly referred to as a spinning mass or wheel which tends to hold its position in a space-referenced orientation set due to the principle of conservation of angular momentum
gyroscopes
These gyroscopes use the principle of conservation of angular momentum to provide a positional or attitude reference: typically aircraft pitch position, roll position or yaw position (heading).
position gyroscopes
These gyroscopes use the property of precession which allows body rates to be sensed.
rate gyroscopes
Due to the property of _, gyroscopes can be used to provide information relating to the aircraft body rates: pitch rate, roll rate and yaw rate.
precession
devices that measure acceleration along a particular axis
accelerometers
The measurement of _ can be integrated using computers used to derive aircraft velocity and position.
acceleration
All _ use the principle of sensing the force on a loosely suspended mass, from which the acceleration may be calculated.
accelerometers
The availability of inertial navigation systems (INS) to the civil aviation community during the late _ added another dimension to the navigation equation.
1960s
The use of the Earth’s _ to sense direction and the use of north-seeking devices to establish the direction of magnetic north for the purposes of navigation is one of the oldest forms of sensor.
magnetic field
provides magnetic heading, and when combined with a directional gyro (DG), which provides an inertial heading reference, can provide a ‘magnetic heading and reference system’ (MHRS)
magnetic sensor or flux-valve
defined as the process of combining data from a number of different sensors to provide information that is not present in the individual sources
sensor fusion/data fusion/multisensor navigation
aims to create a more comprehensive and accurate picture by leveraging the strengths of multiple inputs
sensor fusion/data fusion/multisensor navigation
achieved by having multiple sensors of the same kind that give off the same type of information
redundancy
example of an aircraft that has 3 pitot tubes and 6 static ports
Airbus A320
example of an aircraft that has 3 pitot tubes and 4 static ports
Boeing 737
when multiple sensors of the different types are used together
diverse sensor fusion