AIRCRAFT PILOTING ASSISTANCE SYSTEM AND METHOD

摘要

A piloting assistance system for an aircraft during manual piloting is provided. The piloting assistance system includes a monitoring module, configured to compare an acceleration of the aircraft to an authorized acceleration that depends on a speed of the aircraft, an acceleration control module, able to be switched between an activated state and a deactivated state, and configured so as, in the activated state, excluding the deactivated state, to generate a control signal of at least one control device of the acceleration of the aircraft to push the acceleration of the aircraft toward the authorized acceleration range, in order to keep or push the speed of the aircraft in a predefined usage speed range, the monitoring module being configured to activate the acceleration control module when the acceleration of the aircraft is not comprised in the authorized acceleration range.

主权项

1. An aircraft piloting assistance system during manual piloting of the aircraft, the system comprising:
a monitor configured to compare, at each moment, an acceleration of the aircraft at the moment to an authorized acceleration range for the aircraft at the moment, the authorized acceleration range depending on a speed of the aircraft at the moment, an acceleration controller switchable between an activated state and a deactivated state, the acceleration controller being configured, in the activated state, excluding the deactivated state, to generate a control signal of at least one control device of the acceleration of the aircraft at least at one control moment in order to bring the acceleration of the aircraft toward the authorized acceleration range, in order to keep or bring the speed of the aircraft in or toward a predefined usage speed range, the monitor being configured to activate the acceleration controller at a given activation moment when the acceleration of the aircraft at the given activation moment is not comprised in the authorized acceleration range.