BR0201627B1 - processo para determinar a glissagem lateral de uma aeronave usando uma sonda de dados aeronáuticos e uma unidade de referência inercial, e, sistema para determinar a glissagem lateral de uma aeronave tendo uma unidade de referência inercial que proporciona informação inercial de vôo - Google Patents

processo para determinar a glissagem lateral de uma aeronave usando uma sonda de dados aeronáuticos e uma unidade de referência inercial, e, sistema para determinar a glissagem lateral de uma aeronave tendo uma unidade de referência inercial que proporciona informação inercial de vôo

Info

Publication number
BR0201627B1
BR0201627B1 BRPI0201627-3B1A BR0201627A BR0201627B1 BR 0201627 B1 BR0201627 B1 BR 0201627B1 BR 0201627 A BR0201627 A BR 0201627A BR 0201627 B1 BR0201627 B1 BR 0201627B1
Authority
BR
Brazil
Prior art keywords
glissing
aircraft
lateral
determining
reference unit
Prior art date
Application number
BRPI0201627-3B1A
Other languages
English (en)
Other versions
BR0201627A (pt
Inventor
Kevin Glenney
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 filed Critical
Publication of BR0201627A publication Critical patent/BR0201627A/pt
Publication of BR0201627B1 publication Critical patent/BR0201627B1/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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • G05D1/0204—Control of position or course in two dimensions specially adapted to aircraft to counteract a sudden perturbation, e.g. cross-wind, gust

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)
  • Navigation (AREA)
  • Measuring Fluid Pressure (AREA)
BRPI0201627-3B1A 2001-05-08 2002-05-07 processo para determinar a glissagem lateral de uma aeronave usando uma sonda de dados aeronáuticos e uma unidade de referência inercial, e, sistema para determinar a glissagem lateral de uma aeronave tendo uma unidade de referência inercial que proporciona informação inercial de vôo BR0201627B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/850,863 US6561020B2 (en) 2001-05-08 2001-05-08 Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information

Publications (2)

Publication Number Publication Date
BR0201627A BR0201627A (pt) 2003-03-11
BR0201627B1 true BR0201627B1 (pt) 2013-07-09

Family

ID=25309305

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0201627-3B1A BR0201627B1 (pt) 2001-05-08 2002-05-07 processo para determinar a glissagem lateral de uma aeronave usando uma sonda de dados aeronáuticos e uma unidade de referência inercial, e, sistema para determinar a glissagem lateral de uma aeronave tendo uma unidade de referência inercial que proporciona informação inercial de vôo

Country Status (7)

Country Link
US (1) US6561020B2 (pt)
EP (1) EP1256863B1 (pt)
JP (1) JP2003043056A (pt)
BR (1) BR0201627B1 (pt)
CA (1) CA2383844C (pt)
DE (1) DE60238292D1 (pt)
IL (1) IL149304A (pt)

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US7379839B2 (en) * 2002-12-23 2008-05-27 Rosemount Aerospace, Inc. Multi-function air data probes employing neural networks for determining local air data parameters
US6772080B2 (en) * 2002-12-24 2004-08-03 The Boeing Company System and method for kinematic consistency processing
US7127335B2 (en) * 2003-03-25 2006-10-24 Rosemount Aerospace Inc. Low airspeed assist algorithm for air data computer applications
US6928341B2 (en) * 2003-05-13 2005-08-09 The Boeing Company Computational air data system for angle-of-attack and angle-of-sideslip
US7257470B2 (en) * 2004-10-29 2007-08-14 Rosemount Aerospace Inc. Fault isolation method and apparatus in artificial intelligence based air data systems
US7213454B2 (en) * 2005-04-06 2007-05-08 Rosemount Aerospace Inc. Method and apparatus for obtaining improved accuracy and range for air data parameters inferred from independent measurements of interdependent pressures
FR2892699B1 (fr) 2005-10-27 2008-02-08 Airbus France Sas Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef
US20070130096A1 (en) * 2005-12-01 2007-06-07 Rosemount Aerospace, Inc. Fault detection in artificial intelligence based air data systems
FR2911682B1 (fr) * 2007-01-23 2009-03-06 Airbus France Sas Dispositif et procede d'estimation de la pression statique d'une masse d'air en vue notamment de la determination de la vitesse d'un aeronef dans cette masse d'air.
IT1392259B1 (it) * 2008-12-11 2012-02-22 Alenia Aeronautica Spa Procedimento di stima dell'angolo di incidenza e dell'angolo di derapata di un aeromobile
FR2945513B1 (fr) * 2009-05-18 2013-02-08 Airbus France Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale
FR2945514B1 (fr) * 2009-05-18 2012-09-28 Airbus France Procede et dispositif pour detecter automatiquement une dissymetrie laterale d'un aeronef
CZ302336B6 (cs) * 2010-01-07 2011-03-16 Ceské vysoké ucení technické - Fakulta elektrotechnická Systém pro korekci nepresností systému inerciální navigace
US8479581B2 (en) 2011-05-03 2013-07-09 General Electric Company Device and method for measuring pressure on wind turbine components
ITTO20130601A1 (it) * 2013-07-16 2013-10-15 Torino Politecnico Sistema e procedimento di misura e valutazione di dati aria e inerziali.
US20160370236A1 (en) * 2015-06-22 2016-12-22 Rosemount Aerospace Inc. Aircraft total air temperature anomaly detection
US9703293B2 (en) * 2015-08-31 2017-07-11 The Boeing Company Aircraft stall protection system
US9932127B2 (en) 2015-12-08 2018-04-03 Rosemount Aerospace Inc. Synthetic air data output generation
US10006801B2 (en) 2016-03-31 2018-06-26 Textron Innovations, Inc. Aircraft weight estimation
US10006928B1 (en) 2016-03-31 2018-06-26 Textron Innovations Inc. Airspeed determination for aircraft
US10852316B2 (en) 2018-06-15 2020-12-01 Rosemount Aerospace Inc. Advanced air data system architecture with air data computer incorporating enhanced compensation functionality
US11015955B2 (en) * 2018-06-15 2021-05-25 Rosemount Aerospace Inc. Dual channel air data system with inertially compensated backup channel
US10913545B2 (en) 2018-06-15 2021-02-09 Rosemount Aerospace Inc. Architecture for providing enhanced altitude functionality to aircraft air data system
US11067593B2 (en) 2018-07-20 2021-07-20 Rosemount Aerospace Inc. Pitot static systems with angle of sideslip determination and compensation
US11154169B2 (en) 2018-08-13 2021-10-26 Omachron Intellectual Property Inc. Cyclonic air treatment member and surface cleaning apparatus including the same
EP4021809B1 (en) * 2019-08-30 2024-08-14 Aerosonic LLC Aircraft airflow sensor having error correction based on aircraft movement and process of correcting said sensor based on aircraft movement

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Also Published As

Publication number Publication date
US6561020B2 (en) 2003-05-13
CA2383844A1 (en) 2002-11-08
US20030015032A1 (en) 2003-01-23
BR0201627A (pt) 2003-03-11
EP1256863B1 (en) 2010-11-17
IL149304A (en) 2005-06-19
EP1256863A3 (en) 2005-05-18
EP1256863A2 (en) 2002-11-13
JP2003043056A (ja) 2003-02-13
CA2383844C (en) 2010-02-02
IL149304A0 (en) 2002-11-10
DE60238292D1 (de) 2010-12-30

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Legal Events

Date Code Title Description
B15K Others concerning applications: alteration of classification

Free format text: ALTERADA A CLASSIFICACAO DE B64C 31/04 PARA B64D 45/00

Ipc: B64D 45/00 (2011.01)

B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 09/07/2013, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 19A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2622 DE 06-04-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.