WO2003104081A1

WO2003104081A1 - A method for the contactless measuring of distance and position in respect of aircraft docking procedures, and an arrangement for this purpose.

Info

Publication number: WO2003104081A1
Application number: PCT/SE2003/000801
Authority: WO
Inventors: Nils-Erik Anderberg
Original assignee: Fmt International Trade Ab
Priority date: 2002-06-11
Filing date: 2003-05-19
Publication date: 2003-12-18
Also published as: AU2003228197A1; SE0201775L; SE520914C2; DE60329291D1; EP1511673A1; SE0201775D0; EP1511673B1; SE520914E; US6704098B2; US20030227610A1; DK1511673T3; ATE442987T1; ES2330325T3

Abstract

A method for the contactless measuring of distances to aircraft when positioning said aircraft, such as when docking or parking said aircraft, wherein a scanning laser (2) belonging to a distance measuring device (1) is directed towards an area along a centre line (3) along which an aircraft (4) is intended to be moved in the positioning of said aircraft and located in a position in front of an aircraft to be positioned, said laser (2) being adapted to emit measuring pulses (6) stepwise or incrementally at different angles so as to detect a predetermined measurement volume.The invention is characterised in that said laser (2) is caused to be calibrated with the distance from the laser (2) to the ground in respect of at least some of said angles; in that the laser (2) is caused to measure the distance at said angles during positioning of an aircraft (4); in that the measured distances are compared with said calibrated distances in a computer (7) belonging to the distance measuring device (1); and in that the laser (2) is considered to have measured the correct distance when there is a predetermined agreement with said calibrated distance.The invention also relates to apparatus for carrying out the inventive method. ?

Description

A METHOD FOR THE CONTACTLESS MEASURING OF DISTANCE AND POSITION IN RESPECT OF AIRCRAFT DOCKING PROCEDURES,

AND AN ARRANGEMENT FOR THIS PURPOSE.

The present invention relates to a method for the contactless measuring of distance and position in respect of aircraft docking procedures, and also to an arrangement for this purpose.

When docking an aircraft to a so-called gate-associated passenger bridge, it is known to measure the distance of the aircraft from the passenger bridge with the aid of a contactless measuring process. This measuring process is also applied in the case of so-called remote parking, i.e. when the aircraft is parked on the apron or hardstanding of a gate area instead of being docked with a passenger bridge. It is also known for the pilot to indicate the position of the aircraft in relation to the centre line along which the aircraft shall move towards a stop point at which the door of the aircraft is located in register with the opening of the passenger bridge, or in some other specific position. The distance measuring procedure is used to indicate said stop point to the pilot. The stop point is individual to different aircraft and is thus located at different distances from the distance measuring device used. Such a docking system is therefore aware of the type of aircraft to be docked and therewith also the distance between the distance measuring device and a specific part of the aircraft.

It is necessary to measure said distance during the whole of the docking phase, in order to present the current distance on a display positioned in front of the pilot, such that the pilot will be able to judge the speed at which the aircraft approaches the stop point. Should the aircraft proceed beyond the stop point, there is a danger of, e.g., an aircraft wing or engine colliding with ground equipment, resulting in highly expensive repair work.

The technology most used at present for measuring said distance and, in certain instances, the position of the aircraft in relation to said centre line, employs the use of distance measuring lasers. Only a small number of companies are active within this field. Certain of these use this technology. The applicant of the instant application and the Swedish company Safegate International AB and RLG Corporation in the U.S.A. are among those companies that use this technology. Honeywell and Siemens are examples of companies that use a video-based technique. The accuracy of a video camera is basically dependent on camera resolution and the measuring distance. Because it is necessary to rely on the contrast between the measured object and the surroundings when using the video-based technique, the result will be influenced by external factors, such as rain, fog, snow and light conditions. The video technique is therefore less efficient.

The laser technique is superior to the video technique, among other things because the measurement obtained will be more exact, by virtue of being highly accurate per se, and also because the measuring points on the measured object, i.e. the aircraft, are small and the surroundings therefore have no real disturbing affect. Moreover, the absolute measuring accuracy does not vary appreciably with distance in the case of laser measuring processes.

However, there is a problem with existing docking systems in which lasers are used. According to international rules and regulations concerning existing equipment, the equipment shall, itself, indicate when the measurements obtained are erroneous. No system that fulfils this requirement with complete satisfaction exists at present. This deficiency of existing systems presents a serious hazard, partly because an erroneous distance indication can be given, and partly because an erroneous indication is not presented to the pilot in control of a docking aircraft. Such defective functions in existing systems have resulted in incidents and accidents.

A known laser system is designed so that the distance measuring laser will measure the distance to a known reference for controlling measurement accuracy and function, for instance the distance to a reflector that is positioned in a direction from the laser that differs from the volume within which the laser measures against a docking aircraft. The laser is considered to have measured correctly, when the reference measurement gives a distance that is in sufficient accord with tie known distance. The measuring procedure is then undertaken solely towards an expected aircraft. The known system does not have the time to check measurement accuracy and function by measuring both against a reflector and carrying out measurements against an aircraft during a docking process at one and the same time. The inability of the known system to perform both of these tasks simultaneously is because the laser is adapted to scan a large number of measuring points in one or two dimensions within the measurement volume, whereas the reference measurement is carried out in a totally different direction. By measurement volume is meant the two-dimensional or three-dimensional space within which the laser scans by emitting respective received laser beams or rays.

Thus, when using this known system there is no knowledge of whether the laser measures the correct distance to an approaching aircraft, or even whether the system measures the distance at all. The laser light emitted may be absorbed by weather conditions that indicate to the laser that the measuring distance lies beyond its range.

The present invention solves this problem.

Thus, the present invention relates to a method for contactless measuring distance to aircraft when positioning the aircraft, such as when docking or parking the aircraft, wherein a scanning laser associated with a distance measuring device is directed towards an area along a central line along which an aircraft is intended to be moved in positioning the aircraft and situated in a position in front of an aircraft being positioned, wherein the laser is adapted to emit measuring pulses stepwise at different angles such as to detect a predetermined measurement volume, and wherein the method is characterised in that said laser is caused to be calibrated with the distance from the laser to the ground in respect of at least some of said angles; in that the laser is caused to measure the distance at said angles during positioning of an aircraft; in that the measured distances are caused to be compared with said calibrated distance in a computer belonging to the distance measuring device; and in that the laser is considered to measure the correct distance when predetermined agreement is reached.

The invention also relates to an arrangement of the kind defined in Claim 10 and having the general characteristic features set forth in said Claim.

The invention will now be described in more detail, partly with reference to the accompanying drawings, in which

- Figure 1 is a side view of an aircraft shown in two different positions;

- Figure 2 shows an aircraft from above in two different positions; - Figure 3 is a schematic block diagram illustrating an inventive arrangement; and

- Figure 4 illustrates schematically a display for providing a pilot with aircraft docking information.

The present invention relates to a method and to an arrangement for the contactless measurement of the distance to an aircraft when positioning said aircraft, such as when docking or parking the aircraft. The arrangement includes a distance measuring device 1 and associated scanning laser. The laser 2 is pointed in the direction of a centre line 3 along which an aircraft 4 is intended to be moved in positioning the aircraft, and is situated in front of the aircraft being positioned. The distance measuring device 1 is normally mounted on a wall 5 of the airport building. Alternatively, it may be mounted on a post or pillar on the airport hardstanding or apron when an aircraft shall be positioned, e.g., parked at a place remote from an airport building.

The laser 2 is adapted to send measurement pulses stepwise at different angles, as illustrated schematically in Figure 1 by lines 6, so as to detect a predetermined measurement volume. Pulse emission is effected with the aid of a laser-carried moveable mirror onto which laser pulses are directed.

Such a laser emits light pulses in small angular increments of 0.125 degrees. Angular increments of 1 (one) degree are shown in Figure 1 for the sake of clarity. The known laser is an eye-safe low-power laser that emits infrared light.

In the example shown in Figure 1, measuring is shown to be effected onto the ground up to a distance A of 100 metres. The shortest measuring distance in Figure 1 is in the order of 25 metres and referenced B, this distance corresponding to a distance of roughly 2 metres in front of the nose wheel of the aircraft 4. This position is the aircraft stop position.

Figure 1 shows the bundle of laser beams or rays 6 within an angle v of 15 degrees. The distance measuring device 1 including the laser 2 may be placed, e.g., at a height of 5-10 metres above ground level. However, laser beams are normally emitted both upwards and downwards, as illustrated in Figure 3. For example, the angle v is 20 degrees upwards and 25 degrees downwards, calculated from the horizontal plane.

According to the invention, the laser 2 is calibrated with the distance from the laser to the ground with respect to at least some of said angles, i.e. along certain of the lines 6. The laser 2 is caused to measure the distance at said angles, during positioning of an aircraft 4. The distances measured are compared with said calibrated distances in a computer 7 belonging to the distance measuring device 1. The laser is considered to have measured the correct distance, when a predetermined agreement is reached.

The laser is calibrated after having been fitted and installed, by measuring the distance to the ground in the absence of disturbing objects along the measurement path. At least some of these measurement values are stored in a memory belonging to the computer 7.

The comparison with the calibrated distances in the computer 7 is made with current measurement values obtained during the ongoing positioning of an aircraft.

As before mentioned, the absolute measurement accuracy does not vary appreciably with the distance in the case of laser measuring processes. This means that it suffices to measure against one or more ground positions.

Known systems for aircraft measuring processes using such laser techniques include software by means of which it can be established that measurements are made against an incoming aircraft.

When an aircraft shall be positioned, the aircraft swings in on the centre line 3, as shown to the right in Figures 1 and 2, for instance.

Measurements are taken at different height zones above the ground, when an aircraft is expected to arrive. In this regard, the laser beams are not directed so as to meet the ground, but are expected to be reflected against an aircraf . Reflection of such beams or rays is considered to indicate that an aircraft has been detected. In this respect, it can be ascertained that different proximal distances are obtained in respect of laser pulses emitted at close angles, this disparity in distance corresponding to the shape of the forward part of the aircraft body.

According to the invention, the distance to the ground is also measured. It is this measuring process that is illustrated in Figure 1. Figure 1 does not illustrate the aforesaid measuring process in different height zones. In the case of the example shown in Figure 1, the uppermost line, corresponding to a given angle, meets the ground beneath the aircraft. If this distance is one of the calibrated distances, it is compared with the stored calibrated distance. The aircraft continues to move to the left in Figure 1. The aircraft will therewith break said uppermost line, wherein the laser will measure a shorter distance than the distance calibrated for this angle. If, however, the laser measures a distance corresponding to the distances calibrated for other angles the laser still measures correctly, and hence the measured shorter distance is measured against an object, i.e. the aircraft. Lines 6 are broken successively as the aircraft continues to move to the left in Figure 1.

As a result of the invention, reference measurements to the ground are made constantly, as a result of the distances actually measured being compared with the known calibrated values.

According to a highly preferred embodiment of the invention, the computer is caused to compare at least some measured distances to the ground and to compare these distances with the calibrated values during the whole of the docking procedure.

Should the laser break down or malfunction, for instance as a result of a computer error, so that the laser will not measure the correct distance at a given angular position in comparison with the calibrated distance, this will be discovered immediately. The same applies should the laser not be able to measure a distance at a given angular position. This may be because the light is not reflected to a sufficient extent or because an object other than an aircraft is present in the aircraft taxiing line, although the absence of a measured distance may equally as well be due to malfunctioning of the distance measuring device.

Solely measuring against an area along the centre line 3 has been dealt with in the aforegoing. In its simplest form, this merely requires the scanning laser to be adapted to scan vertically in one dimension. However, the area may have a certain horizontal width. Moreover, it may be situated to one side of the centre line.

With regard to control measurements made at calibrated angles and distances to the ground, such measurements are meaningless if made on the centre line or on one side of said line.

However, said contactless measurement of distances can also be caused to measure the position of the aircraft relative to said centre line. This can be achieved by causing the scanning laser to scan vertically and horizontally, i.e. in two dimensions. The side of the centre line on which the aircraft may perhaps be displaced can be detected by virtue of the fact that the distances to the front part of the aircraft are not symmetrical with respect to the centre line.

According to a highly important embodiment of the invention, the computer 7 is adapted to send a signal to the positioning system in which the laser 2 is included in the event of a deviation greater than said predetermined agreement, this signal causing an indication to be shown on a display, or corresponding laser connection, that tells the pilot that the positioning system is out of function.

Figure 4 is a schematic illustration of a known display 8. The laser is marked with a window 9 through which laser beams are sent and received. The reference numeral 10 identifies a leading mark indicator according to Swedish Patent Specification No. 8105509-7, which is based on moare technology. When the aircraft is positioned on the centre line, the pilot sees a vertical black dash 11 on the leading mark indicator 10. Such known displays 8 also include text fields in which the type of aircraft is given, among other things. These displays are often connected 13 to a data system which is central to the airport and in which information concerning the type of aircraft to be positioned is found, among other things. When the aircraft has reached its stop point, this is indicated by the word "STOP" presented in the text field 12.

An indication to the pilot that the positioning system is out of function is suitably effected precisely by causing the computer 7 to display the word "STOP" in the text field of the display 8. This information can be stored in a so-called log-file in the docking system computers and can also be sent to other computer systems both inside and outside the airport.

In Figure 3, the line 14 denotes the highest directed laser beam for distance measuring, and the line 15 denotes the most downwardly directed laser beam.

According to one preferred embodiment, the laser 2 is aligned so that its measurement volume will include the emission of measurement pulses onto the ground, even when an expected aircraft 4 has reached its stop point during the positioning process. This is illustrated in Figure 1 with the beams or rays 13 that strike the ground in front of the nose wheel when the aircraft is in its left position.

According to one embodiment, the laser 2 is aligned so that measurement against the ground occurs only beyond the point, as seen from the laser, at which the apron or hardstanding shall be vacant for the aircraft concerned. It may be so that vehicles and pieces of equipment are located closest to the laser, i.e. between the aircraft stop point and the aircraft structure. In such a case, it may be so that the laser measures the distance to a vehicle or piece of equipment. This distance would not coincide with a corresponding calibrated distance and a false error indication would be shown on the display 8.

According to another embodiment, the maximum measuring distance is determined on a measuring occasion by measuring the distance to the ground, for instance at the commencement of an aircraft positioning process. The distance measuring device 5 is then caused to ignore measurement values in respect of objects or the like at distances further away than said maximum measuring distance during the aircraft positioning process.

Although the invention has been described above with reference to a number of exemplifying embodiments, it will be understood that the invention can be modified with respect to the choice of laser, the choice of angle areas, and so on, without departing from the basic concept of the invention. For instance, the function and measuring accuracy of the distance measuring device can be checked against the calibrated distance values that have been obtained when measuring the ground distance, during the distance measuring process. It will therefore be understood that the invention is not restricted to the aforedescribed and illustrated exemplifying embodiments thereof and that variations can be made within the scope of the accompanying Claims.

Claims

1. A method for the contactless measuring of distances to aircraft in the process of positioning said aircraft, such as when docking or parking said aircraft, wherein a scanning laser (2), associated with a distance measuring device (1), is directed towards an area along a centre line (3) along which an aircraft (4) is intended to be moved in the positioning of said aircraft, and is located in front of an aircraft to be positioned, said laser (2) being adapted to emit measuring pulses (6) stepwise at different angles so as to detect a predetermined measurement volume, characterised in that said laser (2) is caused to be calibrated with the distance from the laser (2) to the ground in respect of at least some of said angles; in that the laser (2) is caused to measure the distance at said angles during positioning of an aircraft (4); in that the measured distances are compared with said calibrated distances in a computer (7) belonging to the distance measuring device (1); and in that the laser (2) is considered to have measured the correct distance when there is a predetermined agreement with said calibrated distance.

2. A method according to Claim 1, characterised in that said contactless measuring of distances is also caused to measure the lateral position of the aircraft (4) relative to said centre line (3).

3. A method according to Claim 1 or 2, characterised in that in the event of a deviation greater than said predetermined agreement said computer (7) is caused to send to the positioning system in which the laser (2) is included a signal which presents on a display (8) or the like in connection with the laser an indication to the pilot that the positioning system is out of function.

4. A method according to Claim 1, 2 or 3, characterised by aligning the laser (2) so that its measurement volume will include measurement pulses transmitted onto the ground even when an expected aircraft (4) has reached its stop point during the aircraft positioning process.

5. A method according to Claim 4, characterised in that said computer (7) is caused to compare at least certain measured distances to the ground and compare these measured values with the calibrated values during the entire aircraft positioning process.

6. A method according to Claim 1, 3, 4 or 5, characterised in that the scanning laser (2) is adapted to scan in a vertical plane.

7. A method according to Claim 1, 2, 3, 4 or 5, characterised in that the scanning laser (2) is adapted to scan in a vertical plane and in a horizontal plane.

8. A method according to Claim 1, 2, 3, 4, 5, 6 or 7, characterised in that the laser (2) is aligned so that measuring the distance to the ground takes place solely beyond the point at which the apron or hardstanding shall be free (vacant) for the aircraft (4), as seen from the laser.

9. A method according to any one of the preceding Claims, characterised in that the maximum distance is determined on the measuring occasion by measuring the distance to the ground; and in that the distance measuring device (1) is then caused to ignore the measurement values obtained against objects or the like that are located further away than said maximum measurement distances.

10. An arrangement for contactless measuring of the distance to aircraft in an aircraft positioning process, such as when docking or parking an aircraft, wherein said arrangement includes a distance measuring device (1) and a scanning laser (2) which is directed towards an area along a centre line (3) along which an aircraft (4) is intended to be moved in the positioning process and which is located in front of an aircraft to be positioned, said laser (2) being adapted to emit measuring pulses stepwise at different angles such as to detect a predetermined measurement volume, characterised in that said laser (2) is calibrated with the distance of the laser from the ground in respect of at least some of said angles; in that the laser (2) is adapted to measure the distance at said angles during positioning of an aircraft (4); in that a computer (7) associated with the distance measuring device (1) is adapted to compare the measured distances with said calibrated distances; and in that the computer (7) is adapted to treat the measuring result of the laser (2) as a correct distance upon predetermined agreement with said calibrated distance.

11. An arrangement according to Claim 10, characterised in that said computer (7) is adapted to also measure the lateral position of the aircraft (4) relative to said centre line (3) with the aid of said contactless distance measuring process.

12. An arrangement according to Claim 10 or 11, characterised in that in the event of a deviation greater than said predetermined agreement, the computer (7) is adapted to deliver to the positioning system in which the laser (2) is included a signal which causes there to be shown on a display (8) or the like in connection with said laser (2) information which indicates to the pilot that the positioning system is non-functional.

13. An arrangement according to Claim 1 0, 1 1 or 12, characterised in that the laser (2) is directed so that its measurement volume will include measurement pulses that are transmitted onto the ground even when an expected aircraft (4) has reached its stop point during the positioning process.

14. An arrangement according to Claim 13, characterised in that said computer (7) is adapted to compare at least some of the ground measured distances with the calibrated values during the entire aircraft positioning process.

15. An arrangement according to Claim 10, 11, 12, 13 or 14, characterised in that the scanning laser (2) is adapted to scan in a vertical plane.

16. An arrangement according to Claim 10, 11, 12, 13 or 14, characterised in that the scanning laser (2) is adapted to scan in a vertical plane and in a horizontal plane.

17. An arrangement according to Claim 10, 11, 12, 13, 14, 15 or 16, characterised in that the laser (2) is directed so that ground distance measurements will take place solely beyond the point at which the apron or haidstanding shall be left vacant to accommodate said aircraft (4), as seen from the laser.

18. An arrangement according to any one of the preceding Claims, characterised in that the distance measuring device (1) is adapted to measure the maximum measurement distance on the measuring occasion, by measuring against the ground; and in that the distance measuring device (1) is adapted to then ignore measurement values obtained in respect of objects or the like located further away than said maximum measuring distance.