Method for controlling the piloting of an aircraft
First Claim
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1. A method for controlling the piloting of an aircraft comprising the steps of:
- receiving at least one first instruction provided directly by a pilot for modification of the orientation of a current velocity vector of the aircraft,determining a target velocity vector of the aircraft based on said at least one first instruction provided directly by the pilot, anddetermining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received,the method further comprising the following steps of;
receiving an instruction for modification of the orientation of the predetermined target velocity vector,modifying the target velocity vector as a function of said command received, said actuation command being determined on the basis of the thus-modified target velocity vector,displaying, in real time, a first graphic element representing a direction of the target velocity vector, and a second graphic element representing a direction of the current velocity vector, andadjusting a current flight path of the aircraft based on comparison of the target velocity vector and the current velocity vector,wherein said target velocity vector is defined directly by the pilot by directing said first graphic element on a control screen, andwherein said current flight path is adjusted, and said at least one actuator of the aircraft is automatically controlled, based on said target velocity vector directly defined by the pilot, without the pilot having to act directly on said at least one actuator.
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Abstract
A method for controlling the piloting of an aircraft comprising the steps of receiving at least one first instruction for modification of a current velocity vector of the aircraft, determining a target velocity vector of the aircraft, on the basis of said at least one first instruction received, and determining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received.
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Citations
16 Claims
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1. A method for controlling the piloting of an aircraft comprising the steps of:
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receiving at least one first instruction provided directly by a pilot for modification of the orientation of a current velocity vector of the aircraft, determining a target velocity vector of the aircraft based on said at least one first instruction provided directly by the pilot, and determining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received, the method further comprising the following steps of; receiving an instruction for modification of the orientation of the predetermined target velocity vector, modifying the target velocity vector as a function of said command received, said actuation command being determined on the basis of the thus-modified target velocity vector, displaying, in real time, a first graphic element representing a direction of the target velocity vector, and a second graphic element representing a direction of the current velocity vector, and adjusting a current flight path of the aircraft based on comparison of the target velocity vector and the current velocity vector, wherein said target velocity vector is defined directly by the pilot by directing said first graphic element on a control screen, and wherein said current flight path is adjusted, and said at least one actuator of the aircraft is automatically controlled, based on said target velocity vector directly defined by the pilot, without the pilot having to act directly on said at least one actuator. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An aircraft piloting control system comprising
a processing unit configured to receive at least one first instruction provided directly by a pilot for modification of the orientation of a current velocity vector of the aircraft, to determine a target velocity vector of the aircraft based on said at least one first instruction provided directly by the pilot, and to determine, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received, said processing unit being moreover configured to receive an instruction for modification of the orientation of the target velocity vector determined, and modify the target velocity vector as a function of said received command, said actuation command being determined on the basis of the thus-modified target velocity vector, and to display, in real time, a first graphic element representing a direction of the target velocity vector, and a second graphic element representing a direction of the current velocity vector, and adjust a current flight path of the aircraft based on comparison of the target velocity vector and the current velocity vector, wherein said target velocity vector is defined directly by the pilot by directing said first graphic element on a control screen, and wherein said current flight path is adjusted, and said at least one actuator of the aircraft is automatically controlled, based on said target velocity vector directly defined by the pilot, without the pilot having to act directly on said at least one actuator.
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15. A method for controlling the piloting of an aircraft comprising the steps of:
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receiving at least one first instruction provided directly by a pilot for modification of the orientation of a current velocity vector of the aircraft, determining a target velocity vector of the aircraft based on said at least one first instruction provided directly by the pilot, and determining, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received, the method further comprising the following steps of; receiving an instruction for modification of the orientation of the predetermined target velocity vector, modifying the target velocity vector as a function of said command received, said actuation command being determined on the basis of the thus-modified target velocity vector, displaying, in real time, a first graphic element representing a direction of the target velocity vector, and a second graphic element representing a direction of the current velocity vector, and adjusting a current flight path of the aircraft based on comparison of the target velocity vector and the current velocity vector, at least one of; in a manual mode by the pilot, and in an automatic mode by a flight control unit, wherein deviations between the first graphic element and the second graphic element are corrected by the pilot in the manual mode, and are corrected by the flight control unit in the automatic mode, such that the current velocity vector substantially follows the target velocity vector, both velocity vectors being represented by the first and second graphic elements, wherein said target velocity vector is defined directly by the pilot by directing said first graphic element on a control screen, and wherein said current flight path is adjusted, and said at least one actuator of the aircraft is automatically controlled, based on said target velocity vector directly defined by the pilot, without the pilot having to act directly on said at least one actuator.
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16. An aircraft piloting control system comprising
a processing unit configured to receive at least one first instruction provided directly by a pilot for modification of the orientation of a current velocity vector of the aircraft, to determine a target velocity vector of the aircraft based on said at least one first instruction provided directly by the pilot, and to determine, on the basis at least of said target velocity vector, at least one actuation command intended for at least one actuator of the aircraft in order to modify the movement of the aircraft according to said at least one first instruction received, said processing unit being moreover configured to receive an instruction for modification of the orientation of the target velocity vector determined, and modify the target velocity vector as a function of said received command, said actuation command being determined on the basis of the thus-modified target velocity vector, and to display, in real time, a first graphic element representing a direction of the target velocity vector, and a second graphic element representing a direction of the current velocity vector, and adjust a current flight path of the aircraft based on comparison of the target velocity vector and the current velocity vector, at least one of: -
in a manual mode by the pilot, and in an automatic mode by a flight control unit, wherein deviations between the first graphic element and the second graphic element are corrected by the pilot in the manual mode, and are corrected by the flight control unit in the automatic mode, such that the current velocity vector substantially follows the target velocity vector, both velocity vectors being represented by the first and second graphic elements, wherein said target velocity vector is defined directly by the pilot by directing said first graphic element on a control screen, and wherein said current flight path is adjusted, and said at least one actuator of the aircraft is automatically controlled, based on said target velocity vector directly defined by the pilot, without the pilot having to act directly on said at least one actuator.
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Specification