# US 11,113,975 B2 · Method and device for assisting in the piloting of an aircraft to observe a required time of arrival

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- Number: US 11,113,975 B2
- Document ID: US11113975B2
- Status: Granted
- Kind: B2
- Application number: 16/390,127
- Filed: 2019-04-22
- Published: 2019-10-31
- Granted: 2021-09-07
- Earliest claimed: 2018-04-25
- Assignees: Airbus Operations GmbH
- Applicants: Airbus Operations SAS
- Inventors: Thomas Pastre; Jérome Arnoux
- Web page: https://patentgrep.com/patent/US11113975B2

## CPC

- G01C 23/005: {Flight directors (indicating arrangements specially adapted for rotary gyroscopes G01C19/32)}
- G08G 5/30: Flight plan management
- G01C 21/20: Instruments for performing navigational calculations (G01C21/24, G01C21/26 take precedence)
- G05D 1/101: {specially adapted for aircraft}
- G06Q 50/40: Business processes related to the transportation industry (shipping G06Q10/083)
- G08G 5/21: located onboard the aircraft
- G01C 21/10: by using measurements of speed or acceleration (G01C21/24, G01C21/26 take precedence)
- G01C: MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY (measuring liquid level G01F; radio navigation, determining distance or velocity by use of propagation effects, e.g. Doppler effects, propagation time, of radio waves, analogous arrangements using other waves G01S)
- G08G: TRAFFIC CONTROL SYSTEMS (guiding railway traffic, ensuring the safety of railway traffic B61L; arrangement of road signs or traffic signals E01F9/00; radar or analogous systems, sonar systems, lidar systems specially adapted for traffic control G01S13/91, G01S15/88, G01S17/88; {radar or analogous systems, sonar systems, lidar systems specially adapted for anti-collision purposes G01S13/93, G01S15/93, G01S17/93})
- G05D: SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G06Q: INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR

## Abstract

A method for assisting in the piloting of an aircraft to observe a required time of arrival at a waypoint during a flight according to a predetermined flight plan comprising a nominal speed profile, comprising at least two flight segments, comprises the steps of determining an effective speed profile of the aircraft, and controlling by a guidance computer of the aircraft according to the effective speed profile. The step of determining an effective speed profile comprises the substeps of computing, for each segment of the nominal speed profile, a corrective term that is a function of a correction coefficient common to all the segments of the nominal speed profile, and computing, for each segment of the effective speed profile, a setpoint speed equal to the sum of a nominal speed of the nominal speed profile and of the corrective term.

## Claims

### Claim 1

A method for assisting in the piloting of an aircraft in order to observe a required time of arrival at a waypoint during a flight of the aircraft according to a predetermined flight plan, this flight plan comprising a nominal speed profile of the aircraft comprising at least two distinct flight segments for each of which there are defined a nominal flight speed, a maximum flight speed and a minimum flight speed of the aircraft,
the method comprising the following steps implemented by a processing unit of a flight management computer of the aircraft:
a) determination of an effective speed profile of the aircraft, this effective speed profile comprising flight segments similar to those of the nominal speed profile, said determination comprising the following substeps:
a3) computation, for each segment of the nominal speed profile, of a corrective term corresponding to a product of a correction coefficient by a difference between one of the maximum speed or the minimum speed defined for this segment and the nominal speed corresponding to this segment, the correction coefficient being a correction coefficient common to all the segments of the nominal speed profile; and
a4) computation, for each segment of the effective speed profile, of a setpoint speed equal to a sum of the nominal speed defined for a corresponding segment of the nominal speed profile and of the corrective term computed for the corresponding segment of the nominal speed profile,
b) controlling of a guidance computer of the aircraft to guide the aircraft according to the effective speed profile determined in the step a).

### Claim 2 (depends on 1)

The method according to claim 1, wherein step a) comprises a substep a1) of computation of an estimated time of arrival at the waypoint by considering that the aircraft flies according to the nominal speed profile and, in step a3), the difference between one of the maximum speed or the minimum speed defined for the segment and the nominal speed corresponding to this segment is chosen to be equal to:
the difference between the maximum speed and the nominal speed defined for this segment when said estimated time of arrival at the waypoint is later than the required time of arrival; and
the difference between the minimum speed and the nominal speed defined for this segment when said estimated time of arrival at the waypoint is prior to the required time of arrival.

### Claim 3 (depends on 2)

The method according to claim 2, wherein step a) further comprises:
a substep a2), prior to substep a3), of selection of a value of a correction coefficient common to all the segments of the speed profile; and
a substep a5) of computation of an estimated time of arrival at the waypoint by considering that the aircraft flies according to the effective speed profile comprising the setpoint speed values computed in substep a4), and
substeps a2), a3), a4) and a5) are implemented iteratively until the difference between the estimated time of arrival at the waypoint and the required time of arrival is below a predetermined time threshold.

### Claim 4 (depends on 3)

The method according to claim 3, wherein, in substep a2), a value of the correction coefficient common to all the segments of the speed profile is selected by using a dichotomy method.

### Claim 5 (depends on 4)

The method according to claim 4, wherein the dichotomy method is a dichotomy method weighted according to the difference between the estimated time of arrival at the waypoint and the required time of arrival.

### Claim 6 (depends on 1)

The method according to claim 1, wherein a value of the correction coefficient lies between 0 and 1.

### Claim 7

A system for assisting in a piloting of an aircraft in order to observe a required time of arrival at a waypoint during a flight of the aircraft according to a predetermined flight plan, this flight plan comprising a nominal speed profile of the aircraft comprising at least two distinct flight segments for each of which there are defined a nominal flight speed, a maximum flight speed and a minimum flight speed of the aircraft, the system comprising:
a flight management computer which comprises a processing unit configured to determine an effective speed profile of the aircraft, this effective speed profile comprising flight segments similar to those of the nominal speed profile, said determination of the effective speed profile comprising:
a computation, for each segment of the nominal speed profile, of a corrective term corresponding to a product of a correction coefficient by a difference between one of the maximum flight speed or the minimum flight speed defined for this segment and the nominal flight speed corresponding to this segment, the correction coefficient being a correction coefficient common to all segments of the nominal speed profile; and
a computation, for each segment of the effective speed profile, of a setpoint speed equal to a sum of the nominal flight speed defined for the corresponding segment of the nominal speed profile and of the corrective term computed for a corresponding segment of the nominal speed profile,
a guidance computer of the aircraft configured to guide the aircraft according to the effective speed profile determined by the processing unit of the flight management computer.

### Claim 8 (depends on 7)

An aircraft comprising a piloting assistance system according to claim 7.