CA2093546A1 - Procede et dispositif d'anti-collisions terrain pour aeronef - Google Patents

Procede et dispositif d'anti-collisions terrain pour aeronef

Info

Publication number
CA2093546A1
CA2093546A1 CA002093546A CA2093546A CA2093546A1 CA 2093546 A1 CA2093546 A1 CA 2093546A1 CA 002093546 A CA002093546 A CA 002093546A CA 2093546 A CA2093546 A CA 2093546A CA 2093546 A1 CA2093546 A1 CA 2093546A1
Authority
CA
Canada
Prior art keywords
aircraft
altitude
envelope
representing
horizontal components
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
CA002093546A
Other languages
English (en)
Other versions
CA2093546C (fr
Inventor
Xavier Chazelle
Anne-Marie Hunot
Gerard Lepere
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.)
Thales SA
Original Assignee
Xavier Chazelle
Anne-Marie Hunot
Gerard Lepere
Dassault Electronique
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9428589&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CA2093546(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Xavier Chazelle, Anne-Marie Hunot, Gerard Lepere, Dassault Electronique filed Critical Xavier Chazelle
Publication of CA2093546A1 publication Critical patent/CA2093546A1/fr
Application granted granted Critical
Publication of CA2093546C publication Critical patent/CA2093546C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/005—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 with correlation of navigation data from several sources, e.g. map or contour matching
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
    • G01S13/935—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft for terrain-avoidance
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13—Receivers
    • G01S19/14—Receivers specially adapted for specific applications
    • G01S19/15—Aircraft landing systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
    • 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
    • G08G5/0086—Surveillance aids for monitoring terrain
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers

Abstract

Abrégé Procédé et dispositif d'anti-collisions terrain pour aéronef Application comme aide à la navigation aérienne. Une mémoire de masse (30) stocke une base de données (BDT) représentant au moins une partie substantielle du globe terrestre, selon un maillage à plusieurs niveaux, plus précis notamment au voisinage d'un aéroport. Sont reçues des indications d'état, représentant la position de l'aéronef, avec deux composantes horizontales (L,G) et l'altitude (Z), et les vecteurs vitesse et accélération de l'aéronef, ainsi que des indications de commande (MZC) provenant du poste de commande. En fonction desdites composantes horizontales de la position de l'aéronef, des moyens (35) transfèrent en mémoire rapide (40) une carte locale temporaire, à partir de laquelle est définie une enveloppe en altitude du terrain, dans la zone où évolue l'aéronef. Des moyens de traitement anti-collision (4; 43, 46) permettent d'établir une alarme (51) si la relation entre un domaine de protection et l'enveloppe en altitude satisfait une première condition qui est définie au moins en partie par lesdites indications de commande. Figure 4A.
CA002093546A 1992-04-07 1993-04-06 Procede et dispositif d'anti-collisions terrain pour aeronef Expired - Lifetime CA2093546C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9204245A FR2689668B1 (fr) 1992-04-07 1992-04-07 Procede et dispositif d'anti-collisions terrain pour aeronef.
FR9204245 1992-04-07

Publications (2)

Publication Number Publication Date
CA2093546A1 true CA2093546A1 (fr) 1993-10-08
CA2093546C CA2093546C (fr) 2003-12-09

Family

ID=9428589

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002093546A Expired - Lifetime CA2093546C (fr) 1992-04-07 1993-04-06 Procede et dispositif d'anti-collisions terrain pour aeronef

Country Status (11)

Country Link
US (2) US5488563A (fr)
EP (1) EP0565399B1 (fr)
JP (1) JPH0624393A (fr)
AT (1) ATE147869T1 (fr)
CA (1) CA2093546C (fr)
DE (1) DE69307377T2 (fr)
DK (1) DK0565399T3 (fr)
ES (1) ES2099391T3 (fr)
FR (1) FR2689668B1 (fr)
GR (1) GR3022297T3 (fr)
RU (1) RU2124760C1 (fr)

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FR2689668A1 (fr) 1993-10-08
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US5638282A (en) 1997-06-10
GR3022297T3 (en) 1997-04-30
US5488563A (en) 1996-01-30
FR2689668B1 (fr) 1994-05-20
EP0565399A1 (fr) 1993-10-13
CA2093546C (fr) 2003-12-09
RU2124760C1 (ru) 1999-01-10
JPH0624393A (ja) 1994-02-01
ATE147869T1 (de) 1997-02-15
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DE69307377D1 (de) 1997-02-27
DE69307377T2 (de) 1997-07-03

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