ES2180587T3 - Sistema de navegacion aerea. - Google Patents

Sistema de navegacion aerea.

Info

Publication number
ES2180587T3
ES2180587T3 ES94927125T ES94927125T ES2180587T3 ES 2180587 T3 ES2180587 T3 ES 2180587T3 ES 94927125 T ES94927125 T ES 94927125T ES 94927125 T ES94927125 T ES 94927125T ES 2180587 T3 ES2180587 T3 ES 2180587T3
Authority
ES
Spain
Prior art keywords
flashing
camera
navigation system
equipment contains
air navigation
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
ES94927125T
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 ES2180587T3 publication Critical patent/ES2180587T3/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
    • G05D1/04—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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/18—Visual or acoustic landing aids

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Studio Devices (AREA)

Abstract

LA INVENCION SE REFIERE A UN SISTEMA DE NAVEGACION PARA UN AVION CON CAMARA DE TV, QUE PUEDE SER UTILIZADA PARA EL RODAJE, COMIENZO Y ATERRIZAJE DE AVIONES DE CLASES DIFERENTES BAJO CONDICIONES ATMOSFERICAS DIFICILES. UN EQUIPAMIENTO DEL SUELO MUESTRA ADICIONALMENTE A LAS LUCES DE DESTELLO HABITUALES, ES DECIR A UN BALIZAMIENTO CORRESPONDIENTE, LUCES DE DESTELLO DISPUESTAS DE FORMA EMPAREJADA CON UNA LONGITUD DE ONDA DE TRABAJO AMPLIADA. A BORDO DEL AVION SE ENCUENTRA UNA CAMARA TV Y UN EQUIPO DE ELABORACION Y PROCESADO DE SEÑAL. LA CAMARA DE ABORDO RECEPCIONA LAS SEÑALES DE LAS LAMPARAS DE DESTELLO ADICIONALES DISPUESTAS DE FORMA EMPAREJADA. EN EL LADO DE RECEPCION SE EFECTUA UNA SINCRONIZACION CON LA FRECUENCIA DE DESTELLO A TRAVES DE LA VALORACION OPTICA CORRESPONDIENTE, SIN QUE SEA NECESARIO UNA UNION DE ALTA FRECUENCIA ENTRE LOS EQUIPAMIENTOS DE ABORDO Y DE TIERRA. EL EQUIPAMIENTO DE ABORDO POSEE PARA ELLO UNA UNIDAD DE ACCIONAMIENTO PARA CONTROL DE LA DISTANCIA FOCAL DE UN OBJETIVO PARA LA CAMARA, DONDE EL CONTROL SE APLICA SOBRE LAS SEÑALES DE LAS LAMPARAS DE DESTELLO ADICIONALES Y SE OBTIENE EL RESULTADO DEL CALCULO DE PARAMETRO DEL MOVIMIENTO DEL AVION. LOS DATOS NUMERICOS PARA LA POSICION DEL AVION ASI COMO DATOS VISUALES BAJO REFERENCIA SOBRE LAS SEÑALES DE LAMPARA DE DESTELLO SE REPRESENTAN CON UNA UNIDAD DE INDICACION, DE TAL FORMA QUE SE MEJORA LA SEÑAL DE MANIOBRA DEL AVION EN CONDICIONES ATMOSFERICAS EXTREMAS.
ES94927125T 1992-07-10 1994-08-19 Sistema de navegacion aerea. Expired - Lifetime ES2180587T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SU925049778A RU2019472C1 (ru) 1992-07-10 1992-07-10 Телевизионная система для руления, взлета и посадки самолетов в сложных метеоусловиях
PCT/RU1994/000196 WO1996006008A1 (en) 1992-07-10 1994-08-19 Aircraft navigation system

Publications (1)

Publication Number Publication Date
ES2180587T3 true ES2180587T3 (es) 2003-02-16

Family

ID=26653657

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94927125T Expired - Lifetime ES2180587T3 (es) 1992-07-10 1994-08-19 Sistema de navegacion aerea.

Country Status (6)

Country Link
EP (1) EP0776825B1 (es)
AT (1) ATE219738T1 (es)
DE (1) DE59410142D1 (es)
ES (1) ES2180587T3 (es)
RU (1) RU2019472C1 (es)
WO (1) WO1996006008A1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2182313C2 (ru) * 1999-08-25 2002-05-10 Сафьян Дмитрий Анатольевич Комплексная навигационная система для летательных аппаратов различных классов (варианты)
DE10044365A1 (de) * 2000-09-08 2002-04-04 Hans Zapfe Verfahren und Anordnung zum Überwachen von Starts und Landungen von Luftfahrzeugen
RU2225808C2 (ru) * 2002-05-15 2004-03-20 Федеральное государственное унитарное предприятие "Летно-исследовательский институт им. М.М. Громова" Устройство для обеспечения посадки летательного аппарата в ночное время, универсальное, двойного применения (упла-уд)
RU2214943C1 (ru) * 2002-09-16 2003-10-27 Открытое акционерное общество "Корпорация "Фазотрон - научно-исследовательский институт радиостроения" Способ посадки летательного аппарата
RU2519622C2 (ru) * 2012-03-19 2014-06-20 Игорь Николаевич Кочергин Автоматическая инструментальная система передачи метеорологических характеристик аэродрома и ввода их в пилотажно-навигационный комплекс управления полетом самолета
FR3110985A1 (fr) * 2020-05-29 2021-12-03 Airbus Interface homme-machine d’un aéronef en phase de décollage ou d’atterrissage

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3610930A (en) * 1968-12-31 1971-10-05 Texas Instruments Inc Independent infrared landing monitor
DE2324267A1 (de) * 1973-05-14 1974-11-21 Licentia Gmbh Einrichtung zur gesicherten rollfuehrung von flugzeugen auf flughaefen
GB1503646A (en) * 1974-03-29 1978-03-15 Smiths Industries Ltd Display systems
DE2944337A1 (de) * 1979-11-02 1982-06-03 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Anordnung zur automatischen landung eines luftfahrzeuges
DE3629911A1 (de) * 1986-09-03 1988-03-10 Precitronic Landeanflughilfe fuer flugzeuge
US5123615A (en) * 1988-02-03 1992-06-23 Indal Technologies Inc. System and components useful in landing airborne craft
IL88263A (en) * 1988-11-02 1993-03-15 Electro Optics Ind Ltd Navigation system

Also Published As

Publication number Publication date
WO1996006008A1 (en) 1996-02-29
EP0776825B1 (de) 2002-06-26
ATE219738T1 (de) 2002-07-15
DE59410142D1 (de) 2002-08-01
EP0776825A4 (de) 2000-03-22
EP0776825A1 (de) 1997-06-04
RU2019472C1 (ru) 1994-09-15

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