PL407686A1 - Urządzenie do monitorowania lądowania samolotów - Google Patents

Urządzenie do monitorowania lądowania samolotów

Info

Publication number
PL407686A1
PL407686A1 PL407686A PL40768614A PL407686A1 PL 407686 A1 PL407686 A1 PL 407686A1 PL 407686 A PL407686 A PL 407686A PL 40768614 A PL40768614 A PL 40768614A PL 407686 A1 PL407686 A1 PL 407686A1
Authority
PL
Poland
Prior art keywords
aircraft
monitoring
landing
sensors
microprocessor
Prior art date
Application number
PL407686A
Other languages
English (en)
Inventor
Marcin Cebulak
Original Assignee
Ambiton Spółka Z Ograniczoną Odpowiedzialnością
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 Ambiton Spółka Z Ograniczoną Odpowiedzialnością filed Critical Ambiton Spółka Z Ograniczoną Odpowiedzialnością
Priority to PL407686A priority Critical patent/PL407686A1/pl
Priority to US14/433,867 priority patent/US20160257422A1/en
Priority to PCT/PL2014/000033 priority patent/WO2015147660A1/en
Publication of PL407686A1 publication Critical patent/PL407686A1/pl

Links

Classifications

    • 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
    • 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
    • G01S13/882—Radar or analogous systems specially adapted for specific applications for altimeters
    • 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
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/54—Navigation or guidance aids for approach or landing
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/70—Arrangements for monitoring traffic-related situations or conditions
    • G08G5/74—Arrangements for monitoring traffic-related situations or conditions for monitoring terrain

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electromagnetism (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Traffic Control Systems (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

Urządzenie do monitorowania lądowania samolotów wyposażone w system mikroprocesorowy, służący do pomiaru wysokości samolotu nad płytą lotniska w celu prawidłowego przebiegu lądowania charakteryzuje się tym, że urządzenie (5) znajdujące się w samolocie (1) wyposażone jest w system czujników mikroprocesorowych wielokanałowego pomiaru w przedniej części samolotu czujników dziobowych (2) oraz w tylnej części samolotu system czujników ogonowych (3).
PL407686A 2014-03-27 2014-03-27 Urządzenie do monitorowania lądowania samolotów PL407686A1 (pl)

Priority Applications (3)

Application Number Priority Date Filing Date Title
PL407686A PL407686A1 (pl) 2014-03-27 2014-03-27 Urządzenie do monitorowania lądowania samolotów
US14/433,867 US20160257422A1 (en) 2014-03-27 2014-03-31 Device for aeroplane landing monitoring
PCT/PL2014/000033 WO2015147660A1 (en) 2014-03-27 2014-03-31 A device for aeroplane landing monitoring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL407686A PL407686A1 (pl) 2014-03-27 2014-03-27 Urządzenie do monitorowania lądowania samolotów

Publications (1)

Publication Number Publication Date
PL407686A1 true PL407686A1 (pl) 2015-09-28

Family

ID=50771320

Family Applications (1)

Application Number Title Priority Date Filing Date
PL407686A PL407686A1 (pl) 2014-03-27 2014-03-27 Urządzenie do monitorowania lądowania samolotów

Country Status (3)

Country Link
US (1) US20160257422A1 (pl)
PL (1) PL407686A1 (pl)
WO (1) WO2015147660A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110658831B (zh) * 2019-10-22 2022-04-15 深圳市道通智能航空技术股份有限公司 对地高度校正方法及装置、无人飞行器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL312931A3 (en) 1996-02-26 1997-09-01 Stefan Dyrski Method of leading aeroplanes and helicopter down onto ground in any phase of their fight and at any locality
US6012001A (en) * 1997-12-30 2000-01-04 Scully; Robert L. Method and apparatus for determining aircraft-to-ground distances and descent rates during landing
CA2390487C (en) * 2001-06-11 2009-02-10 Robert D. Wiplinger Gear status indicator aircraft landing system
EP2539737A2 (en) * 2010-02-22 2013-01-02 Elbit Systems Ltd. Three dimensional radar system
FR2984577B1 (fr) * 2011-12-16 2014-12-05 Thales Sa Systeme d'assistance au pilotage d'un aeronef, notamment d'aide a l'atterrissage, a l'appontage et a la navigation

Also Published As

Publication number Publication date
WO2015147660A1 (en) 2015-10-01
US20160257422A1 (en) 2016-09-08

Similar Documents

Publication Publication Date Title
MX2017007517A (es) Sensores de impedancia para detectar y monitorear humedad en articulos absorbentes.
EP3348203A4 (en) NONINVASIVE ARTERIOVENOUS PRESSURE MEASURING DEVICE AND ARTERIOVENOUS PRESSURE MEASUREMENT METHOD WITH THE MEASURING DEVICE
MX2017014012A (es) Termopar con conexion a tierra activo y metodo de operacion.
AU2014397779A8 (en) Adjustable dumbbell system having a weight sensor
EP3027150C0 (en) DEVICE FOR ADMINISTRATION OF COMPOSITIONS TO THE EYE
EP3466333A4 (en) BIOMAGNETISM MEASURING DEVICE
BR112017003933A2 (pt) método e sistema para solda
EP2995251A4 (en) MEASURING DEVICE OF INTRAORAL HUMIDITY
EP3173778A4 (en) Dryness/wetness response sensor having high-speed response and high sensitivity
FR3018912B1 (fr) Procede et dispositif d'estimation automatique de parametres lies a un vol d'un aeronef.
SG2013063532A (en) In-flight computing device for aircraft cabin crew
GB201304873D0 (en) Weight measurement device and system for enabling the determination and/or monitoring of alcohol consumption
EP3516898A4 (en) EFFICIENT UPLINK MEASUREMENT SIGNAL RX AND TX WINDOW ALLOCATION WITH TIME MALFUNCTION
PL3589543T3 (pl) Statek powietrzny wyposażony w pomocniczy zespół lotu
FR3004547B1 (fr) Procede et dispositif de detection automatique d'une mesure erronee d'une temperature totale sur un aeronef.
MX351123B (es) Estimacion de señales de llegada directa basadas en señales de llegada directa previstas y mediciones.
IL230249A (en) Autonomous emergency descending and landing of aircraft
SG11201608924SA (en) Method and system for detecting aircraft induced wake turbulence
IN2014CH01287A (pl)
MX2016011265A (es) Faldon aerodinamico de tren de aterrizaje.
IL254751A0 (en) Integrated system to determine turbulent effects, in particular in aircrafts in flight
GB201717994D0 (en) Aircraft wing and wing tip device with fairing
FR3027106B1 (fr) Sonde de mesure de la temperature regnant en sortie de turbine d'helicoptere
FR3021116B1 (fr) Systeme de mesure destine a mesurer la vitesse d'un aeronef
PL407686A1 (pl) Urządzenie do monitorowania lądowania samolotów