System for assisting the pilot of an aircraft by haptic means

System for assisting the pilot of an aircraft according to the preceding claim, characterized in that the seat is furthermore provided with a safety harness (82) also equipped with distributed actuators.

System for assisting the pilot of an aircraft according to the preceding claim, characterized in that the actuators of the harness are vibrators.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the seat comprising lateral returns, actuators with single-axis mini-rams are also distributed in these returns.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the mini-rams being able to move according to a displacement length lying within a predetermined range, at a speed below a predetermined maximum speed and at a frequency below a predetermined maximum frequency, the control means for the actuators or for the groups of actuators comprise means for controlling the length and/or the speed and/or the frequency of displacement.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that it comprises a device (95) for damping the seat.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that it comprises a second seat (80′) intended for a copilot equipped with actuators like the seat of the pilot.

System for assisting the pilot of an aircraft according to the preceding claim, characterized in that the aircraft comprising at least one control stick (70), the system comprises, integrated into each stick (70), a control box (71) linked to the computer and which comprises means for dispatching to the computer control commands for the actuators of the other seat.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the sensors are piloting sensors that is to say sensors of attitude (121), of position (124), of altitude (125), of height (123) and of acceleration (122).

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the sensors are sensors for detecting threats (126).

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the aircraft being equipped with traction means for pulling an external load by means of a cable, the sensors comprise sensors of data regarding angle of the cable relative to the vertical (128), length of the cable (127) and tension of the cable (129).

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that it comprises linked to the computer, a general control panel (20) comprising means for selecting a piloting and/or monitoring and/or training mission, and in that the actuators are controlled by the computer as a function of the mission (or missions) selected.

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that it comprises linked to the computer (50), at least one screen (30, 30′) for displaying graphical information regarding monitoring of the environment of the aircraft (31-36) and/or graphical information regarding piloting and/or training (70, 70′, 37, 38, 38′, 39, 39′).

System for assisting the pilot of an aircraft according to one of the preceding claims, characterized in that the aircraft is an airplane or an helicopter