Which sensors feed an AHRS?

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Multiple Choice

Which sensors feed an AHRS?

Explanation:
An AHRS determines aircraft orientation from its three-axis angular-rate sensors and its three-axis accelerometers. The gyros measure how fast the aircraft is rotating about each axis, providing immediate information about changes in attitude. However, gyro outputs drift over time, so they’re not reliable by themselves for long-term attitude. The accelerometers sense the direction of the total specific force, which, when the aircraft is in steady flight, points toward gravity; this gravity reference helps establish the pitch and roll and provides a long-term correction to gyro drift. By fusing these signals, the system continuously estimates attitude. Heading can be supplied by additional sensors such as a magnetometer, but the essential inputs for the AHRS attitude estimation are the gyros and accelerometers.

An AHRS determines aircraft orientation from its three-axis angular-rate sensors and its three-axis accelerometers. The gyros measure how fast the aircraft is rotating about each axis, providing immediate information about changes in attitude. However, gyro outputs drift over time, so they’re not reliable by themselves for long-term attitude. The accelerometers sense the direction of the total specific force, which, when the aircraft is in steady flight, points toward gravity; this gravity reference helps establish the pitch and roll and provides a long-term correction to gyro drift. By fusing these signals, the system continuously estimates attitude. Heading can be supplied by additional sensors such as a magnetometer, but the essential inputs for the AHRS attitude estimation are the gyros and accelerometers.

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