ES2194027T3 - Sistema de navegacion para helicopteros. - Google Patents

Sistema de navegacion para helicopteros.

Info

Publication number
ES2194027T3
ES2194027T3 ES94927124T ES94927124T ES2194027T3 ES 2194027 T3 ES2194027 T3 ES 2194027T3 ES 94927124 T ES94927124 T ES 94927124T ES 94927124 T ES94927124 T ES 94927124T ES 2194027 T3 ES2194027 T3 ES 2194027T3
Authority
ES
Spain
Prior art keywords
helicopters
navigation system
light beacons
information
unit
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.)
Expired - Lifetime
Application number
ES94927124T
Other languages
English (en)
Inventor
Dmitry Anatolievich Safyan
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of ES2194027T3 publication Critical patent/ES2194027T3/es
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, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • 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
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • B64D45/08—Landing aids; Safety measures to prevent collision with earth's surface optical

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Studio Devices (AREA)

Abstract

LA INVENCION SE REFIERE A UN SISTEMA DE NAVEGACION DE HELICOPTERO, ABARCANDO DOS CAMARAS MONTADAS A BORDO DEL HELICOPTERO. UNA CAMARA ESTA ORIENTADA HACIA ADELANTE MIRANDO HACIA AFUERA, DE FORMA QUE UNA SEGUNDA CAMARA ESTA DIRIGIDA HACIA ABAJO ESENCIALMENTE DE FORMA VERTICAL CON SU EJE OPTICO. SOBRE EL LUGAR DE TERRENO PREVISTO SE DISPONEN EN LAS PUNTAS DE UN TRIANGULO EQUILATERO BALIZAS DE DESTELLO EN EL CONTORNO DEL PUNTO DE TERRENO. LAS SEÑALES OPTICAS SUMINISTRADAS POR LA BALIZA DE DESTELLO SON RECEPCIONADAS POR LAS CAMARAS, DE TAL FORMA QUE A TRAVES DE UN CONMUTADOR Y UN BLOQUE DE SELECCION LAS CAMARAS SON ACTIVABLES EN DEPENDENCIA DE LA POSICION ALCANZADA DEL HELICOPTERO. UN BLOQUE DE CALCULO DE COORDENADAS ACTUA CON UN UNIDAD DE INDICACION O UN MONITOR DE FORMA CONJUNTA Y SIRVE PARA LA DETERMINACION DEL MOMENTO DE SUSPENSION PERMANENTE, DONDE SE DETERMINA ADICIONALMENTE LA VELOCIDAD DE ASCENSO Y ALTURA DEL HELICOPTERO Y SE TIENE EN CUENTA.
ES94927124T 1994-08-19 1994-08-19 Sistema de navegacion para helicopteros. Expired - Lifetime ES2194027T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU1994/000195 WO1996006007A1 (en) 1994-08-19 1994-08-19 Helicopter navigation system

Publications (1)

Publication Number Publication Date
ES2194027T3 true ES2194027T3 (es) 2003-11-16

Family

ID=20129877

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94927124T Expired - Lifetime ES2194027T3 (es) 1994-08-19 1994-08-19 Sistema de navegacion para helicopteros.

Country Status (5)

Country Link
EP (1) EP0776824B1 (es)
AT (1) ATE234222T1 (es)
DE (1) DE59410256D1 (es)
ES (1) ES2194027T3 (es)
WO (1) WO1996006007A1 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19521600A1 (de) * 1995-06-14 1996-12-19 Bodenseewerk Geraetetech Landeverfahren für unbemannte Luftfahrzeuge
DE102007019808A1 (de) * 2007-04-26 2009-06-18 Esg Elektroniksystem- Und Logistik-Gmbh Landehilfesystem für senkrecht startende und landende Luftfahrzeuge, insbesondere Helikopter

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3721499A (en) * 1966-06-30 1973-03-20 Jaureguy J Narbaits Navigating and landing device for aircraft
FR2207059B2 (es) * 1972-11-17 1976-07-23 Thomson Csf
DE2944337A1 (de) * 1979-11-02 1982-06-03 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Anordnung zur automatischen landung eines luftfahrzeuges
CH666576A5 (de) * 1984-09-13 1988-07-29 Olten Ag Elektro Apparatebau Elektrischer apparat.
US4866626A (en) * 1987-09-18 1989-09-12 Egli Werner H Navigation by a video-camera sensed ground array
US5123615A (en) * 1988-02-03 1992-06-23 Indal Technologies Inc. System and components useful in landing airborne craft
US4862164A (en) * 1988-02-09 1989-08-29 The United States Of America As Represented By The Secretary Of The Army Infrared aircraft landing system
FR2636303B1 (fr) * 1988-09-14 1992-05-07 Telecommunications Sa Systeme d'aide a l'appontage d'aeronefs a vol stationnaire sur plate-forme de navire
IL88263A (en) * 1988-11-02 1993-03-15 Electro Optics Ind Ltd Navigation system

Also Published As

Publication number Publication date
DE59410256D1 (de) 2003-04-17
WO1996006007A1 (en) 1996-02-29
EP0776824A4 (de) 2000-03-22
EP0776824B1 (de) 2003-03-12
EP0776824A1 (de) 1997-06-04
ATE234222T1 (de) 2003-03-15

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