Method and device for updating a target altitude for an emergency descent of an aircraft

• US 8,725,322 B2
• Filed: 07/15/2011
• Issued: 05/13/2014
• Est. Priority Date: 07/20/2010
• Status: Active Grant

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Botargues, Paule, Grandperret, Erwin, Burel, Lucas, Bourret, Thierry
• Primary Examiner(s): Jabr, Fadey
• Assistant Examiner(s): Martinez Borrero, Luis A
• Application Number:
  US13/184,174
• Publication Number:
  US 20120022725A1
• Time in Patent Office: 1,033 Days
• Field of Search: 701/3, 701/4, 701/11, 701/14, 701/16, 701/120, 701/408, 701/10, 701/214, 342/15, 342/174, 342/120, 342/357.62, 340/978, 73/17.8
• US Class Current: 701/10
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G05D 1/0055 with safety arrangements
• CPC Class Codes: G05D 1/0688 Emergency descent

Abstract

A method and device are provided for determining a target altitude for an emergency descent of an aircraft that is to be reached by the end of the emergency descent. The device determines an updated target altitude which takes into account variations of barometric pressure and which is able to replace the target altitude that must be reached at the end of the emergency descent. The method includes determining an initial target altitude representative of the initial position of the aircraft and then repeatedly determining a current target altitude along a reference horizontal distance. The current target altitude is compared to the initial target altitude and is used to update the emergency descent if the current target altitude is lower than the initial target altitude.

Claims

1. A method for updating a target altitude for an emergency descent of an aircraft with a target updating device on board the aircraft, the target altitude representing the altitude to be reached by the aircraft at the end of the emergency descent, the method comprising:

(a) determining, with a target security altitude determination device included in the target updating device, a target security altitude as a function of the emergency descent, by automatically and repeatedly carrying out the following operations, from an activation of the emergency descent, and relative to a reference horizontal distance ahead of the aircraft with respect to an initial position of the aircraft at the activation of the emergency descent;

calculating a remaining horizontal distance representing a horizontal distance remaining to be covered by the aircraft from a current position until a position located at the reference horizontal distance;

determining a security altitude corresponding to the remaining horizontal distance;

comparing the security altitude to a threshold altitude; and

selecting, as the target security altitude, a highest value between the security altitude and the threshold altitude, the target security altitude being measured in units of measurement chosen from feet or meters;

(b) calculating, with a correction value calculation device included in the target updating device, a correction value, taking into account variations of barometric pressure occurring during the emergency descent, the correction value being measured in the same units of measurement as the target security altitude and the correction value corresponding to a potential error between an actual current altitude of the aircraft and a measured barometric altitude which is based on a standard reference pressure and is thereby affected by a local QNH pressure of the current position;

(c) arithmetically summing, with an updated target altitude calculation device included in the target updating device, the target security altitude and the correction value to obtain an updated target altitude that replaces the target altitude to be reached before the end of the emergency descent, the updated target altitude being corrected from potential collision risks caused by the potential error between the actual current altitude of the aircraft and the measured barometric altitude; and

(d) transmitting the updated target altitude to an automatic control system of the aircraft to automatically conduct the emergency descent using the updated target altitude.

2. The method according to claim 1, wherein step (b) further comprises:

retrieving from a memory a lowest atmospheric pressure and a highest atmospheric pressure measured in a current day;

calculating, with a difference calculation device, first and second differences between the standard reference pressure and, respectively, the lowest atmospheric pressure and the highest atmospheric pressure; and

selecting a highest difference calculated by the difference calculation device and converting, with a correction conversion device, the highest difference in absolute value into a height value representing the correction value.

3. The method according to claim 1, wherein step (b) further comprises, automatically and repeatedly:

sensing, with a barometric altitude sensor, a current barometric altitude of the aircraft;

sensing, with a sea level height sensor, a current height of the aircraft with respect to sea level, using measurements other than barometric measurement; and

arithmetically subtracting, with a difference calculation device, the current height with respect to sea level from the current barometric altitude so as to obtain the correction value.

4. The method according to claim 1, wherein step (c) further comprises replacing the target altitude with the updated target altitude, repeatedly upon each determination of a new updated target altitude.

5. The method according to claim 1, wherein step (c) further comprises replacing the target altitude with the updated target altitude, only if the updated target altitude is higher than the target altitude.

6. The method according to claim 1, wherein the updated target altitude and the target altitude are repeatedly calculated by calculation pitches, and step (c) further comprises:

calculating a difference between the target altitude for a pitch N−

1, N being an integer, and the updated target altitude for a pitch N;

comparing an absolute value of the calculated difference to a threshold value; and

replacing the target altitude for a pitch N with the updated target altitude for the pitch N, only if the absolute value of the difference is higher than or equal to the threshold value.

7. A process for automatically controlling an emergency descent of an aircraft with an automatic control system on board the aircraft, the process comprising:

(a) determining, with a target security altitude determination device included in a target updating device, a target security altitude as a function of the emergency descent, by automatically and repeatedly carrying out the following operations, from an activation of the emergency descent, and relative to a reference horizontal distance ahead of the aircraft with respect to an initial position of the aircraft at the activation of the emergency descent;

calculating a remaining horizontal distance representing a horizontal distance remaining to be covered by the aircraft from a current position until a position located at the reference horizontal distance;

determining a security altitude corresponding to the remaining horizontal distance;

comparing the security altitude to a threshold altitude; and

selecting, as the target security altitude, a highest value between the security altitude and the threshold altitude, the target security altitude being measured in units of measurement chosen from feet or meters;

(b) calculating, with a correction value calculation device included in the target updating device, a correction value, taking into account variations of barometric pressure occurring during the emergency descent, the correction value being measured in the same units of measurement as the target security altitude and the correction value corresponding to a potential error between an actual current altitude of the aircraft and a measured barometric altitude which is based on a standard reference pressure and is thereby affected by a local QNH pressure of the current position;

(c) arithmetically summing, with an updated target altitude calculation device included in the target updating device, the target security altitude and the correction value to obtain an updated target altitude that replaces the target altitude to be reached before the end of the emergency descent, the updated target altitude being corrected from potential collision risks caused by the potential error between the actual current altitude of the aircraft and the measured barometric altitude;

(d) transmitting the updated target altitude to the automatic control system of the aircraft to automatically conduct the emergency descent using the updated target altitude;

determining automatically, with a vertical setpoint determination device included in the automatic control system, a set of vertical setpoints that includes the updated target altitude representing an altitude to be reached by the aircraft at the end of the emergency descent and a target speed representing a speed that the aircraft should respect during the emergency descent;

determining, with a lateral setpoint determination device included in the automatic control system, a set of lateral setpoints, representing a lateral maneuver to be carried out during the emergency descent; and

guiding the aircraft with an aircraft guidance system included in the automatic control system so that the aircraft simultaneously respects the set of vertical setpoints and the set of lateral setpoints until reaching the updated target altitude.

8. A target updating device for updating a target altitude intended for an emergency descent of an aircraft, the target altitude representing the altitude to be reached by the aircraft at the end of the emergency descent, said target updating device comprising:

a target security altitude determination device that automatically and repeatedly determines a target security altitude as a function of the emergency descent, from an activation of the emergency descent, and relative to a reference horizontal distance ahead of the aircraft with respect to an initial position of said aircraft at the activation of the emergency descent, said target altitude determination device further comprising;

a first element that calculates a remaining horizontal distance, representing a horizontal distance remaining to be covered by the aircraft from a current position until a position located at the reference horizontal distance;

a second element that determines a security altitude corresponding to the remaining horizontal distance;

a third element that compares the security altitude to a threshold altitude; and

a fourth element that selects, as a target security altitude, a highest value between the security altitude and the threshold altitude, the target security altitude being measured in units of measurement chosen from feet or meters;

a correction value calculation device that calculates a correction value taking into account variations of barometric pressure occurring during the emergency descent, the correction value being measured in the same units of measurement as the target security altitude and the correction value corresponding to a potential error between an actual current altitude of the aircraft and a measured barometric altitude which is based on a standard reference pressure and is thereby affected by a local QNH pressure of the current position; and

an updated target altitude calculation device that arithmetically calculates a sum of the target security altitude and the correction value to obtain an updated target altitude that replaces the target altitude to be reached before the end of the emergency descent, the updated target altitude being corrected from potential collision risks caused by the potential error between the actual current altitude of the aircraft and the measured barometric altitude,

wherein the target updating device transmits the updated target altitude via a link to an automatic control system of the aircraft to automatically conduct the emergency descent using the updated target altitude.

10. The target updating device of claim 8, wherein the correction value calculation device calculates the correction value by retrieving from a memory a lowest atmospheric pressure and a highest atmospheric pressure measured in a current day, calculating first and second differences between the standard reference pressure and the lowest atmospheric pressure and the highest atmospheric pressure, respectively, and selecting a highest difference and converting the highest difference in absolute value into a height value representing the correction value.

11. The target updating device of claim 8, wherein the correction value calculation device calculates the correction value by sensing a current barometric altitude of the aircraft, sensing a current height of the aircraft with respect to sea level using measurements other than barometric measurements, and arithmetically subtracting the current height with respect to sea level from the current barometric altitude so as to obtain the correction value.

9. An automatic control system for automatically controlling an emergency descent of an aircraft, comprising:

a target updating device for updating a target altitude intended for an emergency descent of an aircraft, the target altitude representing the altitude to be reached by the aircraft at the end of the emergency descent, said target updating device comprising;

a target security altitude determination device that automatically and repeatedly determines a target security altitude as a function of the emergency descent, from an activation of the emergency descent, and relative to a reference horizontal distance ahead of the aircraft with respect to an initial position of said aircraft at the activation of the emergency descent, said target altitude determination device further comprising;

a first element that calculates a remaining horizontal distance, representing a horizontal distance remaining to be covered by the aircraft from a current position until a position located at the reference horizontal distance;

a second element that determines a security altitude corresponding to the remaining horizontal distance;

a third element that compares the security altitude to a threshold altitude; and

a fourth element that selects, as a target security altitude, a highest value between the security altitude and the threshold altitude, the target security altitude being measured in units of measurement chosen from feet or meters;

a correction value calculation device that calculates a correction value taking into account variations of barometric pressure occurring during the emergency descent, the correction value being measured in the same units of measurement as the target security altitude and the correction value corresponding to a potential error between an actual current altitude of the aircraft and a measured barometric altitude which is based on a standard reference pressure and is thereby affected by a local QNH pressure of the current position; and

an updated target altitude calculation device that arithmetically calculates a sum of the target security altitude and the correction value to obtain an updated target altitude that replaces the target altitude to be reached before the end of the emergency descent, the updated target altitude being corrected from potential collision risks caused by the potential error between the actual current altitude of the aircraft and the measured barometric altitude, wherein the target updating device transmits the updated target altitude via a link to an automatic control system of the aircraft to automatically conduct the emergency descent using the updated target altitude;

a vertical setpoint determination device that automatically determines a set of vertical setpoints including the updated target altitude representing an altitude to be reached by the aircraft at the end of the emergency descent and determined by the target updating device, the target updating device being included in the vertical setpoint determination device;

and the set of vertical setpoints including a target speed representing a speed that the aircraft should respect during the emergency descent;

a lateral setpoint determination device that automatically determines a set of lateral setpoints, representing a lateral maneuver to be carried out during the emergency descent; and

an aircraft guidance system that automatically guides the aircraft so that the aircraft simultaneously respects the set of vertical setpoints and the set of lateral setpoints until reaching the updated target altitude.