Patent attributes
The present disclosure relates to a go-around system for an aircraft. The go-around system includes a controller, an alert system, an auto flight system, and an auto throttle system. The controller is configured to receive flight path information, airspeed information, and runway information from one or more avionic systems, determine, based on the flight path information, airspeed information, and runway information, a go-around advisory, and output an alert signal regarding the go-around advisory. The go-around advisory is a directive to perform a go-around. The alert system is configured to provide at least one of a visual alert, an aural alert, and a detailed information alert to a user in response to receiving the alert signal from the controller. The auto throttle system is configured to automatically adjust a speed of the aircraft for a go-around based on the go-around advisory.
