The flight control indicator with determination of the maximum slope for controlling an aircraft in the bottom a result of flight

摘要

P - flight control indicator for the piloting of an aircraft, followed by ground. - the flight control indicator (1) comprises an assembly (2) of information sources, a calculation unit (3) connected to said assembly (2) of information sources and determining, on the basis of information from said assembly (2) of information sources, at least a maximum total slope of the aircraft, which corresponds to the maximum thrust, and is obtained from the measurement of the performance of the aircraft, extrapolated to the maximum slope and anticipating an engine failure, and a display device (5) high, which has, on a display screen (7), at least one means of indication, which indicates the maximum total slope and which is presented in an environment that exists at the front of the aircraft. / p