Patent US6023665A successfully refreshed from Google Patents.
← Back to Patent Explorer
US6023665A Expired / Lapsed US ⏱️ 0.0 years remaining

Aircraft identification and docking guidance systems

Assignee: ADB Safegate Sweden AB
•
Filing: 1994-10-14
•
Granted: 2000-02-08
•
Expires: 2014-10-14
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A system for detecting, identifying and docking aircraft using laser pulses to obtain a profile of an object in the distance. The system initially scans the area in front of the gate until it locates and identifies an object. Once the identity of the object is known, the system tracks the object. By using the information from the profile, the system can in real time display the type of airplane, the distance from the stopping point and the lateral position of the airplane.

Inventors

  • 👤 Lars Millgard

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 07:23
CPC Classifications
G; G08; G08G; G08G5/00; G08G5/20; G08G5/22; B; B64; B64F; B64F1/00; B64F1/002; B64F1/36; G01; G01S; G01S17/00; G01S17/02; G01S17/06; G01S17/42; G01S17/88; G01S17/89; G01S17/894; G01S7/00; G01S7/48; G01S7/4802; G01S7/481; G01S7/4811; G01S7/497; G08G5/50; G08G5/51; G08G5/70; G08G5/72; G08G5/727

Claims Analysis

Total Claims: 27
Claim 1
Independent Claim 120 words
A system for verifying the shape of a detected object comprising: means for projecting light pulses in angular coordinates onto an object; means for collecting light pulses reflected off said object and for determining the detected shape of said object; means for comparing said detected shape with a profile corresponding to the shape of a known object and for determining whether said detected shape corresponds to said known shape; means for directing said projected light pulses onto a calibration element positioned in a known angular direction and at a known distance from said means for directing said projected light for purposes of calibration of said system; and wherein the means for directing said projected light comprises a second mirror system.
Claim 2
Independent Claim 120 words
A system for verifying the shape of a detected object comprising: means for projecting light pulses in angular coordinates onto an object; means for collecting light pulses reflected off said object and for determining the detected shape of said object; means for comparing said detected shape with a profile corresponding to the shape of a known object and for determining whether said detected shape corresponds to said known shape; means for directing said projected light pulses onto a calibration element positioned in a known angular direction and at a known distance from said means for directing said projected light for purposes of calibration of said system; and wherein the means for directing said projected light comprises a second mirror system.
Claim 3
Dependent Claim 28 words
The system of claim 1 wherein the light pulses are projected onto a mirror system with means for adjusting the mirror system to project the light pulses outwardly.
Claim 4
Dependent Claim 22 words
The system of claim 2 wherein said adjustable mirror system is operated by step motors under the control of a programmed microprocessor.
Claim 5
Dependent Claim 107 words
The system of claim 3 wherein: the microprocessor totals the number of reflected pulses in each scan of said capture zone; said microprocessor determines the largest sum of reflected pulses for three adjacent sectors; and said microprocessor determines that an object has been detected if the largest sum of reflected pulses for three adjacent sectors is at least a predetermined minimum number out of a total number of pulses projected within said three adjacent sectors and the number of reflected pulses in the three sectors with the largest sum is more than half of the total number of reflected pulses in the scan of said capture zone.
Claim 6
Dependent Claim 59 words
The system of claim 1 further including means for tracking an incoming object, said tracking means comprising: means for detecting the position of said incoming object relative to an imaginary axial line projecting from a predetermined point and for detecting the distance between said object and said predetermined point whereby tracking of the location of said object is enabled.
Claim 7
Dependent Claim 76 words
The system of claim 5 wherein: a comparison table is generated containing information about collected light pulses and said information is compared with a profile table indicating the shape of known objects; a distance distribution table is generated recording the distribution of distances from the object to said collection means for each collected light pulse; and an average distance is calculated from the detected position of said object to a desired stopping position for said object.
Claim 8
Dependent Claim 46 words
The system of claim 6 wherein the average distance to the stopping position is calculated by averaging the distance to said stopping position recorded for the entries in the comparison table corresponding to the two adjacent entries in the distance distribution table having the largest sum.
Claim 9
Dependent Claim 33 words
The system of claim 6 wherein the average stopping distance is communicated to a computer on board the aircraft allowing that computer to stop the aircraft when said aircraft reaches said stopping positions.
Claim 10
Dependent Claim 73 words
The system of claim 1 wherein: said light pulses are reflected off said calibration element and are received at a detector; determining a detected angular direction of the element relative to said light source based on said pulses received at said detector and in accordance with predetermined angular parameters; and comparing said detected angular direction with said known angular direction to determine whether said detected angular direction corresponds to said known angular direction.
Claim 11
Dependent Claim 42 words
The system of claim 9 further comprising: means for adjusting the angular parameters if said detected angular direction and said known angular direction do not correspond so that the detected angular direction is caused to correspond essentially to the known angular direction.
Claim 12
Dependent Claim 54 words
The system of claim 9 further comprising: means for determining the detected distance of said calibration element from said light source based on predetermined distance parameters; and comparing said detected distance with a known distance of said calibration element from said light source to determine whether said detected distance corresponds to said known distance.
Claim 13
Dependent Claim 38 words
The system of claim 9 further comprising: means for adjusting the distance parameters if said detected distance and said known distance do not correspond so that the detected distance is caused to correspond essentially to the known distance.
Claim 14
Dependent Claim 54 words
The system of claim 1 wherein the angular direction and distance of said calibration means from said means for directing said projected light in a horizontal plane are calibrated while the angular direction and distance of said calibration means from said means for directing said projected light in a vertical plane are held constant.
Claim 15
Independent Claim 142 words
A system for tracking an incoming object comprising: means for generating light pulses; means for projecting said pulses outwardly onto an incoming object and for reflecting said light pulses off said object; means for collecting the light pulses reflected off of said object; means for detecting the position relative to an imaginary axial line projecting from a predetermined point and for detecting the distance between said object and said predetermined point whereby tracking of the location of said object is enabled; wherein a comparison table is generated reflecting information about the laser scan and is compared with a profile table indicating the shape of known objects; a distance distribution table is generated recording the distribution of distances from the nose of the object to the measuring device for each reflected pulse; and an average distance to a desired stopping position is calculated.
Claim 16
Independent Claim 142 words
A system for tracking an incoming object comprising: means for generating light pulses; means for projecting said pulses outwardly onto an incoming object and for reflecting said light pulses off said object; means for collecting the light pulses reflected off of said object; means for detecting the position relative to an imaginary axial line projecting from a predetermined point and for detecting the distance between said object and said predetermined point whereby tracking of the location of said object is enabled; wherein a comparison table is generated reflecting information about the laser scan and is compared with a profile table indicating the shape of known objects; a distance distribution table is generated recording the distribution of distances from the nose of the object to the measuring device for each reflected pulse; and an average distance to a desired stopping position is calculated.
Claim 17
Dependent Claim 47 words
The tracking system of claim 14 wherein the average distance to the stopping position is calculated by averaging the distance to said stopping position recorded for the entries in the comparison table corresponding to the two adjacent entries in the distance distribution table having the largest sum.
Claim 18
Dependent Claim 32 words
The tracking system of claim 14 wherein a display shows the distance from the object to the stopping point, the type of object and the location of the object compared to center.
Claim 19
Dependent Claim 34 words
The tracking system of claim 14 wherein the average stopping distance is communicated to a computer on board the aircraft allowing that computer to stop the aircraft when said aircraft reaches said stopping position.
Claim 20
Dependent Claim 107 words
An aircraft identification and docking guidance system for verifying the shape of a detected aircraft comprising: an adjustable, non-rotary mirror assembly including a first mirror for continuously projecting laser light pulses outwardly in horizontal planar angular coordinates onto an aircraft and a second mirror for continuously projecting laser light pulses outwardly in vertical planar angular coordinates onto said aircraft; means for collecting light pulses reflected off said aircraft and for determining the detected shape of said aircraft; and means for comparing said detected shape with a profile corresponding to the shape of a known aircraft and for determining whether said detected shape corresponds to said known shape.
Claim 21
Dependent Claim 107 words
An aircraft identification and docking guidance system for verifying the shape of a detected aircraft comprising: an adjustable, non-rotary mirror assembly including a first mirror for continuously projecting laser light pulses outwardly in horizontal planar angular coordinates onto an aircraft and a second mirror for continuously projecting laser light pulses outwardly in vertical planar angular coordinates onto said aircraft; means for collecting light pulses reflected off said aircraft and for determining the detected shape of said aircraft; and means for comparing said detected shape with a profile corresponding to the shape of a known aircraft and for determining whether said detected shape corresponds to said known shape.
Claim 22
Dependent Claim 44 words
The system of claim 18 further including means for directing said projected light pulses onto a calibration element positioned in a known angular direction and at a known distance from said means for directing said projected light for purposes of calibration of said system.
Claim 23
Dependent Claim 18 words
The system of claim 19 wherein the means for directing said projected light comprises a second mirror system.
Claim 24
Independent Claim 140 words
A method for verifying the shape of a detected object comprising: projecting light pulses in angular coordinates onto an object; reflecting said pulses back to a detector and determining the detected shape of the object based on said reflected pulses; comparing said detected shape with a profile corresponding to the shape of a known object; determining whether said detected shape corresponds to said known shape; comparing said detected shape with a profile corresponding to the shape of a known object and for determining whether said detected shape corresponds to said known shape; directing said projected light pulses onto a calibration element positioned in a known angular direction and at a known distance from said means for directing said projected light for purposes of calibration of said system; and wherein means for directing said projected light comprises a second mirror system.
Claim 25
Independent Claim 140 words
A method for verifying the shape of a detected object comprising: projecting light pulses in angular coordinates onto an object; reflecting said pulses back to a detector and determining the detected shape of the object based on said reflected pulses; comparing said detected shape with a profile corresponding to the shape of a known object; determining whether said detected shape corresponds to said known shape; comparing said detected shape with a profile corresponding to the shape of a known object and for determining whether said detected shape corresponds to said known shape; directing said projected light pulses onto a calibration element positioned in a known angular direction and at a known distance from said means for directing said projected light for purposes of calibration of said system; and wherein means for directing said projected light comprises a second mirror system.
Claim 26
Dependent Claim 29 words
The method of claim 21 wherein the profile corresponding to the shape of a known object comprises sets of expected reflected pulses at various distances from the stopping point.
Claim 27
Dependent Claim 14 words
The method of claim 21 wherein a microprocessor is programmed to identify an object.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 2003-02-07 2003-08-09 2004-02-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2007-02-07 2007-08-09 2008-02-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2011-02-07 2011-08-09 2012-02-08 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag