A system for aiding the piloting of an aircraft during a runway approach includes an information source that provides information relating to the aircraft and its environment. A computation unit determines, with the aid of information provided by the information source, an energy reference profile having a trajectory reference profile and a speed reference profile that allows the aircraft to regain a stabilized approach trajectory, if it follows the reference profile. A monitor verifies that the aircraft is following the reference profile. An indicator supplies the pilot with piloting indications for piloting the aircraft so as to follow the reference profile.

 
Web www.patentalert.com

< Flight control system and method of using piezoelectric modal sensors to mitigate flexible body dynamics

> Shock wave modification method and system

> Method and apparatus for fast deploying and retrieving of towed bodies

~ 00573