WO2005081201A1 - Procede de controle de la circulation aerienne - Google Patents

Procede de controle de la circulation aerienne Download PDF

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Publication number
WO2005081201A1
WO2005081201A1 PCT/RU2004/000058 RU2004000058W WO2005081201A1 WO 2005081201 A1 WO2005081201 A1 WO 2005081201A1 RU 2004000058 W RU2004000058 W RU 2004000058W WO 2005081201 A1 WO2005081201 A1 WO 2005081201A1
Authority
WO
WIPO (PCT)
Prior art keywords
airplanes
group
τρeτey
uβd
gρuππe
Prior art date
Application number
PCT/RU2004/000058
Other languages
English (en)
Russian (ru)
Inventor
Valentin Afanasievich Sukholitko
Original Assignee
Sukholitko Valentin Afanasievi
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 Sukholitko Valentin Afanasievi filed Critical Sukholitko Valentin Afanasievi
Priority to PCT/RU2004/000058 priority Critical patent/WO2005081201A1/fr
Priority to EA200400486A priority patent/EA200400486A1/ru
Publication of WO2005081201A1 publication Critical patent/WO2005081201A1/fr

Links

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004Transmission of traffic-related information to or from an aircraft
    • G08G5/0013Transmission of traffic-related information to or from an aircraft with a ground station
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004Transmission of traffic-related information to or from an aircraft
    • G08G5/0008Transmission of traffic-related information to or from an aircraft with other aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047Navigation or guidance aids for a single aircraft
    • G08G5/0052Navigation or guidance aids for a single aircraft for cruising
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0078Surveillance aids for monitoring traffic from the aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0082Surveillance aids for monitoring traffic from a ground station

Definitions

  • the invention relates to the field of aviation, in particular to the means of controlling the movement of aircraft. Izves ⁇ en, vyb ⁇ anny in ⁇ aches ⁇ ve blizhaysheg ⁇ anal ⁇ ga, s ⁇ s ⁇ b u ⁇ avleniya v ⁇ zdushnym movement za ⁇ lyuchayuschiysya in ⁇ m, ch ⁇ with ⁇ m ⁇ schyu vychisli ⁇ eln ⁇ g ⁇ ⁇ m ⁇ le ⁇ sa all v ⁇ zdushnye court na ⁇ dyaschiesya in z ⁇ ne u ⁇ avleniya, ⁇ azdelyayu ⁇ on ⁇ i g ⁇ u ⁇ y in ⁇ azhduyu of ⁇ y ⁇ v ⁇ dya ⁇ v ⁇ zdushnye court ⁇ ebuyuschie u ⁇ avleniya with ve ⁇ ya ⁇ n ⁇ s ⁇ yu, ⁇ avn ⁇ y zero
  • SIGNIFICANT FOX (DR. 26) between aircraft, especially at a height higher than when they are maneuvering, or at any loss of cargo.
  • the technical task of the last resort is to increase the safety of air traffic control.
  • SIGNIFICANT FOX (DR. 26) indi ⁇ a ⁇ a v ⁇ zdushn ⁇ y ⁇ bs ⁇ an ⁇ v ⁇ i ⁇ b ⁇ azhayu ⁇ data ⁇ ass ⁇ yaniya ⁇ ez ⁇ ami, supplying i ⁇ ⁇ mulya ⁇ m s ⁇ v ⁇ zhdeniya on ⁇ m ⁇ b ⁇ azhayu ⁇ in ⁇ matsiyu ⁇ ⁇ a ⁇ ame ⁇ a ⁇ ⁇ n ⁇ li ⁇ n ⁇ y si ⁇ uatsii, ⁇ i e ⁇ m ⁇ ez ⁇ ⁇ d ⁇ ln ⁇ g ⁇ or b ⁇ v ⁇ g ⁇ ⁇ ass ⁇ yaniya in m ⁇ men ⁇ naib ⁇ lsheg ⁇ convergence ⁇ S with d ⁇ ugimi ⁇ S or ⁇ e ⁇ ya ⁇ s ⁇ viyami snabzhayu ⁇ sh ⁇ al ⁇ y, unit length ⁇ y ⁇ avna ⁇ ass ⁇ yaniyu on
  • SIGNIFICANT FOX (DR. 26) ⁇ , on ⁇ ig. 2 shows the spline of the movement of the Verizon® from the city at a time, at 3 The principle of the discipline is shown.
  • ⁇ a ⁇ ig. 1 The following meanings: the complex of information and electronic equipment 1, including the indicators of the air supply; satellite navigation system 2, including receivers and information transmitters and computer components; ⁇ 3 with receivers and information transmitters located on them, as well as computing machines; computational complex ( ⁇ ) 4, including the receiver. and signal transmitters, electronic computers (E ⁇ ) for the processing of payment plans and transmitting transmitting information to a satellite navigation system; communication unit and data transmission 5, including the means of communication (for example, radio communication, satellite communications or the Internet), communication media, communications; 6.
  • the method is implemented by the following method.
  • the signals of the satellite navigation system 2 emitted in the U-band are transmitted to the information receivers located on the ⁇ 3 connected to computing machines.
  • ⁇ ychisli ⁇ elnye machine ⁇ azmeschennye on ⁇ S 3 on ⁇ sn ⁇ vanii
  • b ⁇ vy ⁇ navigatsi ⁇ nny ⁇ sis ⁇ em (na ⁇ ime ⁇ , ⁇ adi ⁇ vys ⁇ me ⁇ a, ba ⁇ vys ⁇ me ⁇ a, izme ⁇ i ⁇ elya s ⁇ s ⁇ i and d ⁇ .)
  • ⁇ asschi ⁇ yvayu ⁇ ge ⁇ g ⁇ a ⁇ iches ⁇ ie ⁇ dina ⁇ y ⁇ S 3 ⁇ ealn ⁇ m v ⁇ emeni and ⁇ e ⁇ edayu ⁇ ⁇ mandu ⁇ e ⁇ eda ⁇ chi ⁇ am in ⁇ matsi
  • SIGNIFICANT FOX (DR. 26) ⁇ luchayu ⁇ signals ⁇ ⁇ e ⁇ eda ⁇ chi ⁇ v in ⁇ matsii, ⁇ azmeschenny ⁇ on ⁇ S 3 and ⁇ e ⁇ edayu ⁇ i ⁇ on vychisli ⁇ elnye ⁇ m ⁇ le ⁇ sy in ⁇ y ⁇ vychisli ⁇ elnye machines ⁇ izv ⁇ dya ⁇ i ⁇ ⁇ b ⁇ ab ⁇ u, ⁇ i e ⁇ m on m ⁇ ni ⁇ a ⁇ vychisli ⁇ elny ⁇ machines ⁇ azhd ⁇ g ⁇ ⁇ S 3 ⁇ b ⁇ azhae ⁇ sya v ⁇ zdushnaya ⁇ bs ⁇ an ⁇ v ⁇ a in ⁇ ealn ⁇ m ⁇ ezhime v ⁇ emeni.
  • the second procedure is skipped on the screen on the screen of the LED indicator, which directly separates the motion from C3.
  • this spline there is a critical distance between the two vessels, which is short of
  • P ⁇ intsi ⁇ g ⁇ adui ⁇ v ⁇ i s ⁇ layna ⁇ v ⁇ emenn ⁇ y sh ⁇ ale for v ⁇ g ⁇ vessel P ⁇ available data ⁇ s ⁇ s ⁇ i and ⁇ a ⁇ zhe ⁇ ⁇ ebuem ⁇ mu v ⁇ emeni g ⁇ adui ⁇ v ⁇ i in LS ⁇ vychislyae ⁇ sya ⁇ ass ⁇ yanie ⁇ abscissa sh ⁇ ale, ⁇ e bude ⁇ s ⁇ ve ⁇ s ⁇ v ⁇ va ⁇ Location of the vessel on the existing spline.
  • ⁇ ⁇ 2 is the corresponding component of the scale of the abscissa, including grapevines, transformers, and the United States. at u 2 - the corresponding components are on a large scale, in the case of the group of companies, converting and turning on the EC, as shown in FIG. 3.
  • the proposed access point of the EC is in the echelon equipped with a drive, as shown in FIG. 2, where is indicated the acceptable wider distance between the two EUs, the significant height between them and the distance between the two EUs is shifted from
  • SIGNIFICANT FOX (DR. 26) points “ ⁇ ” to point “B”.
  • SIGNIFICANT FOX (DR. 26) Area of operations of ATC, as well as more safe maneuvering of the United States.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Traffic Control Systems (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)

Abstract

La présente invention relève du domaine de l'aviation. Le procédé selon l'invention consiste : à déterminer des données instantanées liées aux coordonnées d'aéronefs et à leurs paramètres de trajectoire, à l'aide d'un système de navigation par satellite et/ou d'après les données des systèmes de navigation des aéronefs ; à calculer, après réception desdites données, la tendance de modification des paramètres de vol entre chaque aéronef et l'ensemble des autres aéronefs ; à diviser en trois groupes l'ensemble des aéronefs se trouvant dans la zone de contrôle de la circulation aérienne, à l'aide d'un complexe informatique, en fonction d'une probabilité de nécessité de contrôle. Ladite probabilité est égale à zéro pour le premier groupe, supérieure à zéro mais inférieure à un pour le deuxième groupe, et supérieure à un pour le troisième groupe. Les aéronefs desdits groupes et les données associées sont ensuite affichés sur l'écran d'un dispositif d'affichage, à l'aide de couleurs différentes. Les coordonnées et les paramètres de trajectoire des aéronefs du troisième groupe sont déterminés à des intervalles supérieurs ou égaux à deux secondes, ceux du deuxième groupe sont déterminés à des intervalles deux fois plus longs que pour les aéronefs du troisième groupe, et ceux du premier groupe sont déterminés à des intervalles quatre fois plus longs que pour les aéronefs du troisième groupe. Le traitement et l'affichage des données de vol ne sont effectués que pour les aéronefs se trouvant à une distance ne dépassant pas 250 km.
PCT/RU2004/000058 2004-02-25 2004-02-25 Procede de controle de la circulation aerienne WO2005081201A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PCT/RU2004/000058 WO2005081201A1 (fr) 2004-02-25 2004-02-25 Procede de controle de la circulation aerienne
EA200400486A EA200400486A1 (ru) 2004-02-25 2004-02-25 Способ управления воздушным движением

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU2004/000058 WO2005081201A1 (fr) 2004-02-25 2004-02-25 Procede de controle de la circulation aerienne

Publications (1)

Publication Number Publication Date
WO2005081201A1 true WO2005081201A1 (fr) 2005-09-01

Family

ID=34882013

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2004/000058 WO2005081201A1 (fr) 2004-02-25 2004-02-25 Procede de controle de la circulation aerienne

Country Status (2)

Country Link
EA (1) EA200400486A1 (fr)
WO (1) WO2005081201A1 (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2230316A (en) * 1989-04-14 1990-10-17 Computalog Gearhart Ltd Universal joint arrangement for downhole tools
EP0926511A2 (fr) * 1997-12-15 1999-06-30 Raytheon Company Système pour le contrÔle du trafic aérien
RU2134910C1 (ru) * 1998-03-25 1999-08-20 Крыжановский Георгий Алексеевич Способ управления воздушным движением
US6420993B1 (en) * 1999-08-24 2002-07-16 Raytheon Company Air traffic control system
US20030097216A1 (en) * 2001-11-20 2003-05-22 United Parcel Service Systems and methods for correlation in an air traffic control system of interrogation-based target positional data and GPS-based intruder positional data

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2230316A (en) * 1989-04-14 1990-10-17 Computalog Gearhart Ltd Universal joint arrangement for downhole tools
EP0926511A2 (fr) * 1997-12-15 1999-06-30 Raytheon Company Système pour le contrÔle du trafic aérien
RU2134910C1 (ru) * 1998-03-25 1999-08-20 Крыжановский Георгий Алексеевич Способ управления воздушным движением
US6420993B1 (en) * 1999-08-24 2002-07-16 Raytheon Company Air traffic control system
US20030097216A1 (en) * 2001-11-20 2003-05-22 United Parcel Service Systems and methods for correlation in an air traffic control system of interrogation-based target positional data and GPS-based intruder positional data

Also Published As

Publication number Publication date
EA006094B1 (ru) 2005-08-25
EA200400486A1 (ru) 2005-08-25

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