BR102012019124A2 - Método para melhorar a determinação em tempo real de parâmetros de vôo de uma aeronave, sistema para determinar em tempo real de parâmetros de voo de uma aeronave e aeronave - Google Patents

Método para melhorar a determinação em tempo real de parâmetros de vôo de uma aeronave, sistema para determinar em tempo real de parâmetros de voo de uma aeronave e aeronave

Info

Publication number
BR102012019124A2
BR102012019124A2 BRBR102012019124-5A BR102012019124A BR102012019124A2 BR 102012019124 A2 BR102012019124 A2 BR 102012019124A2 BR 102012019124 A BR102012019124 A BR 102012019124A BR 102012019124 A2 BR102012019124 A2 BR 102012019124A2
Authority
BR
Brazil
Prior art keywords
aircraft
flight parameters
determining
aircraft flight
flight
Prior art date
Application number
BRBR102012019124-5A
Other languages
English (en)
Inventor
Pierre Ezerzere
Georgies Hardier
Cedric Seren
Original Assignee
Airbus Operations Sas
Onera - Off Nat Aerospatiale
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 Airbus Operations Sas, Onera - Off Nat Aerospatiale filed Critical Airbus Operations Sas
Publication of BR102012019124A2 publication Critical patent/BR102012019124A2/pt

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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Evolutionary Computation (AREA)
  • Health & Medical Sciences (AREA)
  • Artificial Intelligence (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)

Abstract

MÉTODO PARA MELHORAR A DETERMINAÇÃO EM TEMPO REAL DE PARÃMETROS DE VOO DE UMA AERONAVE, SISTEMA PARA DETERMINAR EM TEMPO REAL PARÂMETROS DE VOO DE UMA AERONAVE E AERONAVE. Método e sistema para determinação de parãmetros de voo de uma aeronave. De acordo com a invenção, o sistema para determinar, em tempo real, parâmetros de voo de uma aeronave, durante um voo da mesma, compreende um filtro de Kalman estendido (10) que é configurado com base em equações de mecânica de voo, estabelecendo uma relação de dependência entre pelo menos dois parãmetros de voo pré-selecionados de dita aeronave a serem estimados, e que é formado para fornecer, durante o voo de dita aeronave, estimativas conjuntas de ditos parãmetros de voo selecionados.
BRBR102012019124-5A 2011-08-01 2012-07-31 Método para melhorar a determinação em tempo real de parâmetros de vôo de uma aeronave, sistema para determinar em tempo real de parâmetros de voo de uma aeronave e aeronave BR102012019124A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1102405A FR2978858B1 (fr) 2011-08-01 2011-08-01 Procede et systeme pour la determination de parametres de vol d'un aeronef

Publications (1)

Publication Number Publication Date
BR102012019124A2 true BR102012019124A2 (pt) 2014-02-18

Family

ID=46516635

Family Applications (1)

Application Number Title Priority Date Filing Date
BRBR102012019124-5A BR102012019124A2 (pt) 2011-08-01 2012-07-31 Método para melhorar a determinação em tempo real de parâmetros de vôo de uma aeronave, sistema para determinar em tempo real de parâmetros de voo de uma aeronave e aeronave

Country Status (8)

Country Link
US (1) US8682507B2 (pt)
EP (1) EP2555070B1 (pt)
JP (1) JP5982213B2 (pt)
CN (1) CN102981505B (pt)
BR (1) BR102012019124A2 (pt)
CA (1) CA2784186C (pt)
FR (1) FR2978858B1 (pt)
RU (1) RU2012132826A (pt)

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KR102692731B1 (ko) 2020-07-06 2024-08-08 고쿠리츠겐큐카이하츠호진 가이죠·고완·고쿠기쥬츠겐큐죠 엔진의 이상 진단 방법, 엔진의 이상 진단 프로그램을 기록한 컴퓨터로 읽을 수 있는 기억 매체 및 엔진의 이상 진단 시스템
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CN117829016A (zh) * 2023-12-15 2024-04-05 北京特种机械研究所 一种大翼展无人机降落轨迹预测方法及装置

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Also Published As

Publication number Publication date
JP2013049408A (ja) 2013-03-14
CN102981505B (zh) 2016-12-07
EP2555070B1 (fr) 2014-11-26
EP2555070A1 (fr) 2013-02-06
US8682507B2 (en) 2014-03-25
US20130035809A1 (en) 2013-02-07
JP5982213B2 (ja) 2016-08-31
RU2012132826A (ru) 2014-02-10
CA2784186C (fr) 2019-04-23
CA2784186A1 (fr) 2013-02-01
FR2978858A1 (fr) 2013-02-08
CN102981505A (zh) 2013-03-20
FR2978858B1 (fr) 2013-08-30

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]