RU95103976A - Устройство для предотвращения летательного аппарата - Google Patents

Устройство для предотвращения летательного аппарата

Info

Publication number
RU95103976A
RU95103976A RU95103976/11A RU95103976A RU95103976A RU 95103976 A RU95103976 A RU 95103976A RU 95103976/11 A RU95103976/11 A RU 95103976/11A RU 95103976 A RU95103976 A RU 95103976A RU 95103976 A RU95103976 A RU 95103976A
Authority
RU
Russia
Prior art keywords
inclination
gear
trajectory
landing
flying
Prior art date
Application number
RU95103976/11A
Other languages
English (en)
Other versions
RU2153195C1 (ru
Inventor
Фэвр Франсуа
Fr]
Денуаз Ксавье
Original Assignee
Секстант Авьоник (FR)
Секстант Авьоник
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 Секстант Авьоник (FR), Секстант Авьоник filed Critical Секстант Авьоник (FR)
Publication of RU95103976A publication Critical patent/RU95103976A/ru
Application granted granted Critical
Publication of RU2153195C1 publication Critical patent/RU2153195C1/ru

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
    • G08G5/025—Navigation or guidance aids
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)

Abstract

Изобретение относится к устройствам предупреждения столкновений летательных аппаратов, преимущественно столкновений с землей, путем регулирования угла наклона траектории при заходе на посадку. Устройство содержит систему 21 определения местоположения ЛА, базу данных 22, первое средство сравнения 23, средство 24 определения координат точки приземления на ВПП, средство расчета 25 вектора действительного наклона траектории ЛА, средство 26 определения вектора теоретического наклона траектории ЛА и второе средство сравнения 27 двух векторов наклона. Устройство может быть использовано для реализации стадии захода на посадку авиалайнеров.

Claims (1)

  1. Изобретение относится к устройствам предупреждения столкновений летательных аппаратов, преимущественно столкновений с землей, путем регулирования угла наклона траектории при заходе на посадку. Устройство содержит систему 21 определения местоположения ЛА, базу данных 22, первое средство сравнения 23, средство 24 определения координат точки приземления на ВПП, средство расчета 25 вектора действительного наклона траектории ЛА, средство 26 определения вектора теоретического наклона траектории ЛА и второе средство сравнения 27 двух векторов наклона. Устройство может быть использовано для реализации стадии захода на посадку авиалайнеров.
    Figure 00000001
RU95103976/28A 1994-03-22 1995-03-20 Устройство для предотвращения столкновений летательного аппарата RU2153195C1 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9403343A FR2717934B1 (fr) 1994-03-22 1994-03-22 Dispositif d'évitement de collisions pour aéronef notamment avec le sol par contrôle de pente d'approche.
FR9403343 1994-03-22

Publications (2)

Publication Number Publication Date
RU95103976A true RU95103976A (ru) 1996-12-10
RU2153195C1 RU2153195C1 (ru) 2000-07-20

Family

ID=9461300

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95103976/28A RU2153195C1 (ru) 1994-03-22 1995-03-20 Устройство для предотвращения столкновений летательного аппарата

Country Status (7)

Country Link
US (1) US5608392A (ru)
EP (1) EP0674300B1 (ru)
JP (1) JPH07257494A (ru)
CA (1) CA2144808A1 (ru)
DE (1) DE69517725T2 (ru)
FR (1) FR2717934B1 (ru)
RU (1) RU2153195C1 (ru)

Families Citing this family (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2731824B1 (fr) * 1995-03-17 1997-05-16 Sextant Avionique Dispositif d'evitement de collisions pour aeronef notamment avec le sol
ES2112760B1 (es) * 1995-06-06 1998-12-16 Sextant Avionique Dispositivo de prevencion de colisiones para aeronave, spbre todo con el suelo, por control de la pendiente de aproximacion.
US5839080B1 (en) * 1995-07-31 2000-10-17 Allied Signal Inc Terrain awareness system
US6606034B1 (en) * 1995-07-31 2003-08-12 Honeywell International Inc. Terrain awareness system
US6691004B2 (en) 1995-07-31 2004-02-10 Honeywell International, Inc. Method for determining a currently obtainable climb gradient of an aircraft
US6292721B1 (en) * 1995-07-31 2001-09-18 Allied Signal Inc. Premature descent into terrain visual awareness enhancement to EGPWS
US6092009A (en) 1995-07-31 2000-07-18 Alliedsignal Aircraft terrain information system
US6038498A (en) * 1997-10-15 2000-03-14 Dassault Aviation Apparatus and mehod for aircraft monitoring and control including electronic check-list management
US5978715A (en) * 1997-10-15 1999-11-02 Dassault Aviation Apparatus and method for aircraft display and control
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US6057786A (en) * 1997-10-15 2000-05-02 Dassault Aviation Apparatus and method for aircraft display and control including head up display
US6049756A (en) * 1997-11-12 2000-04-11 Lockheed Martin Corporation System and method for avoiding collision between vector and solid objects
FR2783912B1 (fr) 1998-09-24 2001-01-12 Dassault Electronique Dispositif d'aide a l'atterissage, notamment pour l'inhibition d'alerte anti-collision sol
EP1121678B1 (en) 1998-10-16 2004-06-16 Universal Avionics Systems Corporation Flight plan intent alert system and method
AU2150100A (en) * 1998-11-20 2000-06-13 Amsaad, Inc. Minimum safe altitude system and method
WO2000038131A2 (en) * 1998-12-11 2000-06-29 Alliedsignal Inc. Method and apparatus for automated runway selection
WO2000047948A1 (en) * 1999-02-01 2000-08-17 Honeywell International Inc. Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway
US6477449B1 (en) 1999-02-01 2002-11-05 Honeywell International Inc. Methods, apparatus and computer program products for determining a corrected distance between an aircraft and a selected runway
DE60041810D1 (de) 1999-02-01 2009-04-30 Honeywell Int Inc Bodennähe-warnsystem
US6445310B1 (en) 1999-02-01 2002-09-03 Honeywell International, Inc. Apparatus, methods, computer program products for generating a runway field clearance floor envelope about a selected runway
US6484071B1 (en) 1999-02-01 2002-11-19 Honeywell International, Inc. Ground proximity warning system, method and computer program product for controllably altering the base width of an alert envelope
US6785594B1 (en) * 1999-03-25 2004-08-31 Honeywell International Inc. Ground proximity warning system and method having a reduced set of input parameters
US6469664B1 (en) 1999-10-05 2002-10-22 Honeywell International Inc. Method, apparatus, and computer program products for alerting surface vessels to hazardous conditions
US6734808B1 (en) 1999-10-05 2004-05-11 Honeywell International Inc. Method, apparatus and computer program products for alerting submersible vessels to hazardous conditions
US7587278B2 (en) 2002-05-15 2009-09-08 Honeywell International Inc. Ground operations and advanced runway awareness and advisory system
US7117089B2 (en) 2001-03-06 2006-10-03 Honeywell International Inc. Ground runway awareness and advisory system
US8145367B2 (en) 2001-03-06 2012-03-27 Honeywell International Inc. Closed airport surface alerting system
US6769645B1 (en) * 2001-10-11 2004-08-03 Mac Truong Electronic automatic repulsion system
US7206698B2 (en) 2002-05-15 2007-04-17 Honeywell International Inc. Ground operations and imminent landing runway selection
US20040254728A1 (en) * 2002-10-25 2004-12-16 Poropat George Vladimir Collision warning system and method
US7633410B2 (en) * 2004-02-19 2009-12-15 Honeywell International Inc. Wireless assisted recovery systems and methods
FR2875916B1 (fr) * 2004-09-28 2015-06-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef a voilure tournante au voisinage d'un point de pose ou de decollage
FR2878060B1 (fr) * 2004-11-15 2010-11-05 Airbus France Procede et dispositif d'alerte et d'evitement de terrain pour un aeronef
FR2895098B1 (fr) * 2005-12-20 2008-06-20 Thales Sa Systeme embarque de prevention des collisions d'un aeronef avec le terrain
FR2895072B1 (fr) 2005-12-20 2008-02-29 Thales Sa Procede permettant d'eviter les confusions de pistes d'atterrissage
FR2935524B1 (fr) * 2008-08-29 2010-10-01 Thales Sa Dispositif et procede de surveillance de la localisation des aeronefs au sol
US8116923B2 (en) * 2009-11-19 2012-02-14 Honeywell International Stabilized approach monitor
FR2978282B1 (fr) 2011-07-22 2013-08-30 Thales Sa Procede et dispositif pour le filtrage d'alertes provenant d'un systeme de detection de collision d'un aeronef
US9734726B2 (en) * 2014-02-17 2017-08-15 The Boeing Company Systems and methods for providing landing exceedance warnings and avoidance
US9522742B2 (en) * 2014-03-18 2016-12-20 The Boeing Company Short landing warning
RU2557871C1 (ru) * 2014-05-14 2015-07-27 Сергей Михайлович Мужичек Устройство для предотвращения выкатывания воздушных судов за пределы взлетно-посадочной полосы
FR3032044B1 (fr) 2015-01-28 2020-07-17 Airbus Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi.
US9630669B2 (en) 2015-02-04 2017-04-25 Christopher Slaughter Dynamic cycle light distribution system
US11113978B2 (en) * 2016-09-14 2021-09-07 Honeywell International Inc. System and method for determining and displaying optimized aircraft energy level
US11393344B2 (en) * 2017-09-15 2022-07-19 Ntt Docomo, Inc. Flight control apparatus and flight control system
FR3072948B1 (fr) * 2017-10-30 2019-11-15 Airbus Operations Systeme d’aide a l’atterrissage d’un aeronef en phase d’approche d’une piste d’atterrissage
GB2579191B (en) * 2018-11-22 2022-07-13 Ge Aviat Systems Ltd Method and system to identify and display suspcious aircraft
FR3111120B1 (fr) * 2020-06-04 2022-04-29 Airbus Operations Sas Système de vision de vol amélioré pour aéronef.
CN114610078B (zh) * 2022-05-12 2022-08-12 四川腾盾科技有限公司 一种无人机空中航路冲突预警方法及系统

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3752967A (en) * 1971-12-20 1973-08-14 C Vietor Ascent and descent slope tracker system
US4164340A (en) * 1973-03-19 1979-08-14 The Boeing Company Method and apparatus for determining when a glide slope signal exceeds a predetermined level
US3922637A (en) * 1974-10-03 1975-11-25 Sundstrand Data Control Aircraft landing approach ground proximity warning system
US4399425A (en) * 1981-01-12 1983-08-16 Rockwell International Corporation Circuit for operating a flight navigation indicator
US4567483A (en) * 1982-12-10 1986-01-28 Sundstrand Data Control, Inc. Position based ground proximity warning system for aircraft
US4675823A (en) * 1983-12-09 1987-06-23 Sundstrand Data Control, Inc. Ground proximity warning system geographic area determination
US4646244A (en) * 1984-02-02 1987-02-24 Sundstrand Data Control, Inc. Terrain advisory system
US4796190A (en) * 1986-06-04 1989-01-03 Cummings Elihu C Navigation system
US4792906A (en) * 1986-08-29 1988-12-20 The Boeing Company Navigational apparatus and methods for displaying aircraft position with respect to a selected vertical flight path profile
US4914436A (en) * 1987-04-06 1990-04-03 Sundstrand Data Control, Inc. Ground proximity approach warning system without landing flap input
DE3930862A1 (de) * 1989-09-15 1991-03-28 Vdo Schindling Verfahren und einrichtung zur darstellung von flugfuehrungsinformation
FR2689668B1 (fr) * 1992-04-07 1994-05-20 Dassault Electronique Procede et dispositif d'anti-collisions terrain pour aeronef.
CA2099953C (fr) * 1992-07-24 2006-11-14 Engin Oder Procede et dispositif d'assistance au pilotage d'un aerodyne a partir d'un ensemble volumineux de documents stockes en memoire
FR2697796B1 (fr) * 1992-11-10 1994-12-09 Sextant Avionique Dispositif d'évitement de collisions pour aéronef notamment avec le sol.

Also Published As

Publication number Publication date
JPH07257494A (ja) 1995-10-09
EP0674300A1 (fr) 1995-09-27
EP0674300B1 (fr) 2000-07-05
FR2717934A1 (fr) 1995-09-29
FR2717934B1 (fr) 1996-04-26
US5608392A (en) 1997-03-04
DE69517725T2 (de) 2001-03-01
RU2153195C1 (ru) 2000-07-20
CA2144808A1 (fr) 1995-09-23
DE69517725D1 (de) 2000-08-10

Similar Documents

Publication Publication Date Title
RU95103976A (ru) Устройство для предотвращения летательного аппарата
CA1317010C (en) Ground proximity approach warning system without landing flap input
JP3619628B2 (ja) 走行環境認識装置
ATE244895T1 (de) Autonomes landeführungssystem
ES2612163T3 (es) Procedimiento y sistema de dirección de un vehículo aéreo no tripulado
US7917254B2 (en) Aircraft guidance using localizer capture criteria for rectilinear displacement data
EP0351654A3 (en) High accuracy coordinate conversion method for air traffic control applications
US20060271250A1 (en) Approach guidance system and method for airborne mobile platform
EP0738874A3 (en) Navigation display with bird's-eye perspective
EP0790487A3 (en) Aircraft terrain advisory system
EP1243457A3 (en) Tracking of a target vehicle using adaptive cruise control
US9696123B2 (en) Method for focusing a high-energy beam on a reference point on the surface of a flying object in flight
Beall et al. Optic flow and visual analysis of the base-to-final turn
US3911436A (en) Device for aircraft trajectory guidance
US3237194A (en) Image producing apparatus
JP2600503Y2 (ja) 航空機の自動着陸装置
RU1777300C (ru) Способ посадки планирующей парашютной системы на наземный радиомаяк
Dieffenbach Autonomous Precision Approach and Landing System(APALS super (TM))
Van Cott An Optical System for Manned Vehicle Terminal Guidance
LAW et al. A study of a collision avoidance system mounted on a curved ground plane(Semiannual Report)
RU94018425A (ru) Система контроля посадки летательных аппаратов
RU1816723C (ru) Способ обеспечени посадки летательного аппарата
GB1118961A (en) Terrain-following system
HOFFMANN et al. Some test results on the visibility of obstacle and hazard beacons
RU93013548A (ru) Способ формирования сигналов управления летательным аппаратом или судном при движении его по прямой, образованной несколькими радиоконтрастными ориентирами