EP0415587A2 - Système de suivi à avertissement précoce - Google Patents

Système de suivi à avertissement précoce Download PDF

Info

Publication number
EP0415587A2
EP0415587A2 EP90308833A EP90308833A EP0415587A2 EP 0415587 A2 EP0415587 A2 EP 0415587A2 EP 90308833 A EP90308833 A EP 90308833A EP 90308833 A EP90308833 A EP 90308833A EP 0415587 A2 EP0415587 A2 EP 0415587A2
Authority
EP
European Patent Office
Prior art keywords
predefined
height
plane
zone
intrusion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP90308833A
Other languages
German (de)
English (en)
Other versions
EP0415587B1 (fr
EP0415587A3 (en
Inventor
Patrick R. Williams
Mark J. Rentmeesters
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of EP0415587A2 publication Critical patent/EP0415587A2/fr
Publication of EP0415587A3 publication Critical patent/EP0415587A3/en
Application granted granted Critical
Publication of EP0415587B1 publication Critical patent/EP0415587B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0082—Surveillance aids for monitoring traffic from a ground station

Definitions

  • This invention relates generally to computerized methods to provide early warning of collision for a tracking system and pertains more particularly to a process for predicting the probability that an object being tracked will intrude into a predefined polygonal zone.
  • a variety of computerized systems have been developed that are capable of predicting if and when an approaching object will intrude into a predefined region of space. Such systems are typically employed to protect secure zones, such as, for example military installations, to enable appropriate counter measures to be invoked on a timely basis. In addition, these systems are employed in air traffic control systems to assist air traffic controllers in discerning which amongst a potentially large number of objects being tracked are likely to present the possibility of a collision with the ground, restricted airspace or off designated air routes.
  • Performance of previous systems especially those with relatively simple tracking and collision prediction algorithms, often is limited in that in order to solve the probabilities presented by modern vehicle performance envelopes and a relatively large number of closely spaced vehicles being tracked, large amounts of calculations are performed for too many of the objects being tracked. Since the data processing resources available are generally limited, this naturally serves to limit the number of objects such systems can process and increases the probability that false alarms of intrusion or collision will increase, especially when the objects are moving at high speeds, or are capable of rapid and unpredicted changes in path. All of these limitations are exacerbated by uncertainties in the positon or velocities of the vehicle being tracked.
  • a significant aspect of the shortcomings of some prior art systems is the manner in which the uncertainty of positional determinations and velocity vector determinations are accommodated in the calculations.
  • buffer zones are placed both inside and outside the predefined polygonal region to be protected to take into consideration the probable extent of potential tracking errors. If a tracked object is predicted to pierce the inside zone, then a sure lateral intrusion is declared. If, on the other hand, a tracked object is predicted not to pierce the outside zone, then a sure non-intrusion is declared. An unsure intrusion is declared if the object is predicted to penetrate somewhere between the peripheries of the inside and outside buffer zones. The problem with this method is determining the actual boundaries of the buffer zones. An accurate construction of the zones based on track variances has proved intractable. Not only do such systems have trouble accommodating large numbers of objects, especially ones moving at high velocities, but often false alarms and undetected intrusions result.
  • the general purpose of the invention is to provide an early warning tracking system that is quickly able to discern whether an approaching object will intrude into a predefined polygonal zone.
  • the present invention first projects an uncertainty region in the instantaneous direction of travel of each approaching object and then makes decisions regarding the potential for intrusion, depending on the location of the predefined polygonal zone and its relationship to the location of the uncertainty region.
  • the coordinate system is reoriented along the velocity vector for each approaching object.
  • the new coordinates of the periphery of the predefined polygonal zone resulting from the reorientation are then considered with respect to the uncertainty region of each approaching object.
  • the limits of the uncertainty regions are determined by the variances associated with the positional and dynamic determinations of the objects being tracked.
  • the potential for intrusion is first considered in two dimensions to simplify processing. If no lateral intrusion is indicated, no further consideration is given to that particular object. Only after a possible lateral intrusion is indicated, is the object's perceived height and rate of change of height considered to further determine whether an intrusion into the predefined polygonal zone is probable.
  • Fig. 1 generally illustrates the situation and conditions for which the deployment of the system and methods of the present invention are intended.
  • Schematically illustrated in a top plan view is the airspace in and around a predefined polygonal region 61 (having vertices 69-74) in which a multitude of objects are moving at different speeds and directions. Each such object's position is depicted by a dot 63 while its velocity vector, depicted by an arrow 65, is an indication of the speed and direction of its trajectory.
  • This system and its methods can for example assist air traffic controllers in monitoring and controlling the air space in and around a busy airport by directing attention to only those aircraft that are on direct approach, or, help prioritize the deployment of countermeasures for the protection of a restricted military zone.
  • Figure 2 illustrates the overall flow of decisions and logic employed to issue a timely alert regarding an impending intrusion.
  • the system of the present invention Upon detection of the presence of an object by an associated tracking system, the system of the present invention first makes a determination 91 whether the object is sure to intrude laterally, will surely not intrude laterally, or might intrude laterally. This determination is based on the object's perceived position and track velocity as projected onto a horizontal plane presumes that it will not deviate from its flight path and also takes into consideration the uncertainty inherent in the tracking measurements. At this point only the lateral intrusion into the predefined region is of concern and therefore, position and movement are considered only in two dimensions as depicted in Figure 1.
  • the tracking system provides an object's position (x,y) in a horizontal plane as well as its horizontal velocity vector (X,Y). If the object's perceived track speed is below a predefined level: X2 + Y2 ⁇ Q1 (1) the object is considered to be moving too slowly to warrant attention and no further processing is performed. If however the object's track speed is above the predefined level Q1, processing continues by reorienting the entire coordinate system along the object's velocity vector to simplify subsequent calculations.
  • Figure 4 illustrates an object at 75 approaching a predefined polygonal region 79.
  • the position of each vertex (80-83) of the region 79 is initially defined by (a i ,b i ) coordinates.
  • each vertex is redefined as (A i ,B i ) while the object's position would necessarily be defined by (O,O).
  • This reorientation is accomplished as follows: Once reoriented in this fashion it is a simple matter to determine whether an object is approaching or departing from the predefined region. A positive A i indicates an approach while a negative A i is indicative of the object's departure from the particular vertex. If: A i ⁇ O for all i (4) then the object is moving away from the entire predefined region and no further processing is performed for such an object.
  • a J parameter is calculated for each vertex using the vertex's reoriented coordinates (A i ,B i ) as well as the position variance (P), velocity variance (V) and position-velocity covariance (C) as follows:
  • the uncertainty of the object's positional and velocity measurements are interrelated in the denominator of Equation 5 and in effect serve to project an uncertainty zone 84 out in front of the moving object 78 as illustrated in Figure 5.
  • a number of different combinations and permutations are then possible regarding the relationship of a particular predefined region relative to the uncertainty zone 84, i.e., the region can either lie wholly outside 85,86 or wholly inside 87 the zone 84. Alternatively, the region 88,89 can lie partly inside and partly outside the zone or the region 90 can wholly envelope the uncertainty zone.
  • the next step for either a sure intrusion 90 or an unsure intrusion (87, 88, 89) condition entails calculating the lateral entry time 93 of the approaching object 78 into the predefined polygonal region. This is accomplished by considering the vertex closest to the approaching object i.e. the smallest A i which shall be designated A j .
  • the maximum look-ahead time T max is a predefined parameter while the minimum look ahead time is the longer of either a predefined parameter Q4 based on the response time of an appropriate counter measure or a function of how quickly the approaching object can climb over the top of the predefined polygonal region:
  • h (T1) is the predicted height of the approaching object at time T1, which is the predicted time of lateral entry.
  • HU is the upper height limit of the predefined region and ⁇ is a predefined escape climb rate parameter.
  • T1 > T max no alert is indicated. If T1 ⁇ T min , processing continues towards the height final alert process 105. If T1 is in between T min and T max , then processing continues towards height decision alert process 103.
  • the time delay filter 97 is invoked when an unsure intrusion (87, 88, 89) had been indicated in the lateral intrusion determination 91. If T1 > T min then no alert is indicated. If T1 ⁇ T min , processing continues on towards the height final alert process 105.
  • a decision whether to indicate an alert condition or not is made depending on whether missed detections are to be controlled at the expense of false alarms or vice versa. If missed detections are to be controlled at the expense of false alarms, and if: J i > Q7 for any i (16) then processing continues. Otherwise no alert is issued. If on the other hand, false alarms are to be controlled at the expense of missed detections, a second predefined parameter Q8 is considered and if for any two indices j and k: J j > Q8 (17) J k > Q8 (18) and the sign of B j equals the sign of B k then processing continues. Otherwise no alert is issued.
  • the entry time of lateral intrusion T1 As well as the exit time of lateral intrusion T2.
  • the knowledge that an approaching object is above the predefined region at the time of lateral entry does not preclude the possibility of an intrusion. It must therefore also be determined whether the approaching object still has sufficient altitude at the time the predefined polygonal zone is laterally exited.
  • the lateral exit time T2 is calculated 101 in a manner analogous to the calculation of the entry time T1 93.
  • the vertex furthest from the approaching object i.e.
  • the height variance HP, height rate variance HV and height-height rate covariance HC are considered in conjunction with the upper height limit HU and lower height limit HL to provide the final decisions regarding the potential for intrusion.
  • E1 Q10 (HP + 2HC ⁇ T1 + HV ⁇ T12) 1/2 (23)
  • E2 Q11 (HP + 2HC ⁇ T + HV ⁇ T12) 1/2 (24) wherein Q10 and Q11 are predefined parameters.
  • an alert will be issued at 105 if any of the following conditions (equations 29-32) are satisfied: HL ⁇ h + H ⁇ T1 ⁇ HU (29) HL ⁇ h + H ⁇ T2 ⁇ HU (30) h + H ⁇ T1 ⁇ HU and h + H ⁇ T2 ⁇ HL (31) h + H ⁇ T1 ⁇ HL and h + H ⁇ T2 ⁇ HU (32) otherwise no alert will be issued.
  • the alert is turned off if a lateral sure non-intrusion is indicated (Equations 7 & 8) or if either of the following conditions regarding the approaching objects height dynamics are indicated: HL - E1 > h + H ⁇ T1 and HL - E2 > h + H ⁇ T2 (33) HV + E1 ⁇ h + H ⁇ T1 and HU + E2 ⁇ h + H ⁇ T2 (34)
  • the system and methods of the present invention are employed in conjunction with a tracking system which is capable of supplying positional as well as dynamic data for a plurality of moving objects.
  • the perimeter of the predefined polygonal zone is precisely known. The first consideration made is whether a particular object is moving fast enough and in fact toward the predefined polygonal zone. Each object that survives these two considerations then in effect has an uncertainty region projected along its velocity vector.
  • the predefined polygonal zone is then considered in relation to the uncertainty region and depending on its positional relationship the determination whether a sure intrusion exists, a sure non-intrusion exists, or an unsure intrusion is indicated can then be made. If an intrusion is possible, the time for lateral entry and exit is calculated after which the height position and dynamics are taken into consideration.
  • the various parameters employed in the various calculations and determinations are selected according to the requirements of a specific installation. Appropriate adjustment of the values of these various parameters will ultimately determine whether tracking errors will tend to yield false alarms or undetected intrusions.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)
EP19900308833 1989-08-29 1990-08-10 Système de suivi à avertissement précoce Expired - Lifetime EP0415587B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US40025889A 1989-08-29 1989-08-29
US400258 1989-08-29

Publications (3)

Publication Number Publication Date
EP0415587A2 true EP0415587A2 (fr) 1991-03-06
EP0415587A3 EP0415587A3 (en) 1992-12-23
EP0415587B1 EP0415587B1 (fr) 1996-01-03

Family

ID=23582869

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19900308833 Expired - Lifetime EP0415587B1 (fr) 1989-08-29 1990-08-10 Système de suivi à avertissement précoce

Country Status (6)

Country Link
EP (1) EP0415587B1 (fr)
AU (1) AU612082B1 (fr)
CA (1) CA2022313A1 (fr)
DE (1) DE69024563T2 (fr)
FI (1) FI904196A0 (fr)
HK (1) HK105496A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19843799A1 (de) * 1998-09-24 2000-03-30 Euro Telematik Gmbh Verfahren und Anordnung zur Verringerung der Kollisionsgefahr von Luftfahrzeugen
EP1517281A2 (fr) * 2003-09-16 2005-03-23 COMSOFT GmbH Réseau de sécurité pour prévenir de situations dangereuses dans la circulation aérienne

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4196474A (en) * 1974-02-11 1980-04-01 The Johns Hopkins University Information display method and apparatus for air traffic control
WO1988001086A2 (fr) * 1986-07-28 1988-02-11 Hughes Aircraft Company Procede de prediction et de determination d'alertes conflictuelles relatives aux trajectoires de vol d'aeronefs
EP0283723A2 (fr) * 1987-03-06 1988-09-28 International Business Machines Corporation Procédé d'indication d'information à N-dimensions pour le contrôle du trafic aérien
EP0351654A2 (fr) * 1988-07-21 1990-01-24 International Business Machines Corporation Procédé de transformation de coordonnées à haute précision pour des applications de contrôle du trafic aérien
EP0380460A2 (fr) * 1989-01-23 1990-08-01 International Business Machines Corporation Détection et résolution de conflit entre objets en mouvement

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4196474A (en) * 1974-02-11 1980-04-01 The Johns Hopkins University Information display method and apparatus for air traffic control
WO1988001086A2 (fr) * 1986-07-28 1988-02-11 Hughes Aircraft Company Procede de prediction et de determination d'alertes conflictuelles relatives aux trajectoires de vol d'aeronefs
EP0283723A2 (fr) * 1987-03-06 1988-09-28 International Business Machines Corporation Procédé d'indication d'information à N-dimensions pour le contrôle du trafic aérien
EP0351654A2 (fr) * 1988-07-21 1990-01-24 International Business Machines Corporation Procédé de transformation de coordonnées à haute précision pour des applications de contrôle du trafic aérien
EP0380460A2 (fr) * 1989-01-23 1990-08-01 International Business Machines Corporation Détection et résolution de conflit entre objets en mouvement

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19843799A1 (de) * 1998-09-24 2000-03-30 Euro Telematik Gmbh Verfahren und Anordnung zur Verringerung der Kollisionsgefahr von Luftfahrzeugen
EP1517281A2 (fr) * 2003-09-16 2005-03-23 COMSOFT GmbH Réseau de sécurité pour prévenir de situations dangereuses dans la circulation aérienne
EP1517281A3 (fr) * 2003-09-16 2005-06-01 COMSOFT GmbH Réseau de sécurité pour prévenir de situations dangereuses dans la circulation aérienne

Also Published As

Publication number Publication date
DE69024563T2 (de) 1996-09-05
DE69024563D1 (de) 1996-02-15
CA2022313A1 (fr) 1991-03-01
AU612082B1 (en) 1991-06-27
FI904196A0 (fi) 1990-08-24
EP0415587B1 (fr) 1996-01-03
EP0415587A3 (en) 1992-12-23
HK105496A (en) 1996-06-28

Similar Documents

Publication Publication Date Title
EP2669706B1 (fr) Systèmes et procédés pour afficher des informations à évitement d'obstacles lors d'opérations de surface
EP2235711B1 (fr) Systèmes et procédés anticollision à capteurs multiples
US9881508B2 (en) Collision detection system
US5566074A (en) Horizontal miss distance filter system for suppressing false resolution alerts
EP0277229B1 (fr) Procede de prediction et de determination d'alertes conflictuelles relatives aux trajectoires de vol d'aeronefs
US6097996A (en) Method for the lateral avoidance of a mobile zone by a vehicle
US7030780B2 (en) Method for displaying position of an aircraft in a display for air traffic control
US6683541B2 (en) Vertical speed indicator and traffic alert collision avoidance system
US5523759A (en) In flight doppler weather radar wind shear detection system
EP2669703B1 (fr) Systèmes et procédés de filtrage d'informations de capteur de bout d'aile
US20020075171A1 (en) System and method for predicting and displaying wake vortex turbulence
EP1273930B1 (fr) Méthode pour éviter et atténuer des collisions
CA2315330A1 (fr) Systeme et procede permettant de classer et de localiser les aeronefs et les vehicules sur un aeroport
WO1992022830A1 (fr) Systeme radar de detection de cisaillement de vent effectuant un balayage superieur et un balayage inferieur en site
AU7069100A (en) Air traffic control system
CN111276011A (zh) 一种多跑道飞行程序运行的安全评估告警方法及系统
JP2000132799A (ja) 制御対象選別装置
EP0415587B1 (fr) Système de suivi à avertissement précoce
EP0695426B1 (fr) Systeme de detection de cisaillement du vent par radar meteorologique doppler embarque
JP3576031B2 (ja) ビン設定処理装置、ビン設定処理方法及び航空機監視システム
Gazit et al. Aircraft collision avoidance based on GPS position broadcasts
JP3157087B2 (ja) ジャミング発生源検出装置
Watnick et al. Airport movement area safety system
Murugan et al. TCAS functioning and enhancements
JPH04246800A (ja) 後方乱気流警報装置

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): CH DE GB LI SE

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): CH DE GB LI SE

17P Request for examination filed

Effective date: 19930528

17Q First examination report despatched

Effective date: 19950327

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): CH DE GB LI SE

REF Corresponds to:

Ref document number: 69024563

Country of ref document: DE

Date of ref document: 19960215

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: ISLER & PEDRAZZINI AG PATENTANWAELTE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCAR

Free format text: ISLER & PEDRAZZINI AG;POSTFACH 1772;8027 ZUERICH (CH)

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20090813

Year of fee payment: 20

Ref country code: GB

Payment date: 20090827

Year of fee payment: 20

Ref country code: DE

Payment date: 20090821

Year of fee payment: 20

Ref country code: CH

Payment date: 20090825

Year of fee payment: 20

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20100809

EUG Se: european patent has lapsed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20100809

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20100810