IL149304A - Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information - Google Patents

Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information

Info

Publication number
IL149304A
IL149304A IL14930402A IL14930402A IL149304A IL 149304 A IL149304 A IL 149304A IL 14930402 A IL14930402 A IL 14930402A IL 14930402 A IL14930402 A IL 14930402A IL 149304 A IL149304 A IL 149304A
Authority
IL
Israel
Prior art keywords
sideslip
static pressure
calculate
effects
inertial information
Prior art date
Application number
IL14930402A
Other languages
English (en)
Other versions
IL149304A0 (en
Original Assignee
Rosemount Aerospace Inc
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 Rosemount Aerospace Inc filed Critical Rosemount Aerospace Inc
Publication of IL149304A0 publication Critical patent/IL149304A0/xx
Publication of IL149304A publication Critical patent/IL149304A/xx

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)
IL14930402A 2001-05-08 2002-04-23 Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information IL149304A (en)

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
IL149304A0 IL149304A0 (en) 2002-11-10
IL149304A true IL149304A (en) 2005-06-19

Family

ID=25309305

Family Applications (1)

Application Number Title Priority Date Filing Date
IL14930402A IL149304A (en) 2001-05-08 2002-04-23 Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information

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)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CZ201011A3 (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
US10913545B2 (en) 2018-06-15 2021-02-09 Rosemount Aerospace Inc. Architecture for providing enhanced altitude functionality to aircraft air data system
US11015955B2 (en) * 2018-06-15 2021-05-25 Rosemount Aerospace Inc. Dual channel air data system with inertially compensated backup channel
US10852316B2 (en) 2018-06-15 2020-12-01 Rosemount Aerospace Inc. Advanced air data system architecture with air data computer incorporating enhanced compensation functionality
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
KR20220046703A (ko) * 2019-08-30 2022-04-14 에어로소닉 엘엘씨 항공기 움직임을 기초로 한 오류 교정을 갖는 항공기 기류 센서 및 항공기 움직임을 기초로 한 상기 센서의 교정 프로세스

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3318146A (en) 1966-02-14 1967-05-09 Rosemount Eng Co Ltd Pressure sensing instrument for aircraft
US4096744A (en) 1975-09-05 1978-06-27 Rosemount Inc. Pressure sensor for determining airspeed, altitude and angle of attack
US4378696A (en) 1981-02-23 1983-04-05 Rosemount Inc. Pressure sensor for determining airspeed altitude and angle of attack
US4378697A (en) 1981-07-06 1983-04-05 Rosemount Inc. Strut mounted multiple static tube
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
CA2101853C (en) 1991-03-22 2000-08-08 Michael T. Peterson Continuously curved strut mounted sensor
US5205169A (en) 1991-08-08 1993-04-27 Rosemount Inc. Angle of attack sensor using inverted ratio of pressure differentials
FI96260C (fi) 1993-10-29 1996-05-27 Rautaruukki Oy Suodatusmenetelmä ja suodatin
US5616861A (en) * 1995-06-07 1997-04-01 Rosemount Aerospace Inc. Three pressure pseudo -Δ-P sensor for use with three pressure air data probe
US5790405A (en) * 1995-07-31 1998-08-04 Litton Systems, Inc. Method and apparatus for detecting circular torpedo runs
US5852237A (en) * 1997-05-28 1998-12-22 Lockheed Martin Corporation Apparatus and method for measuring the side slip of a low observable aircraft
JP2884502B2 (ja) * 1997-06-03 1999-04-19 科学技術庁航空宇宙技術研究所長 四角錐台型５孔プローブを用いた広速度域飛行速度ベクトル計測システム
US6273370B1 (en) * 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements

Also Published As

Publication number Publication date
US6561020B2 (en) 2003-05-13
CA2383844C (en) 2010-02-02
IL149304A0 (en) 2002-11-10
DE60238292D1 (de) 2010-12-30
BR0201627B1 (pt) 2013-07-09
EP1256863A2 (en) 2002-11-13
EP1256863B1 (en) 2010-11-17
EP1256863A3 (en) 2005-05-18
JP2003043056A (ja) 2003-02-13
US20030015032A1 (en) 2003-01-23
BR0201627A (pt) 2003-03-11
CA2383844A1 (en) 2002-11-08

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