ES2002936A6 - Metodo de determinacion del angulo de ruta por medio de un magnetometro de tres ejes montado fijamente en un avion y de calibracion automatica de dicho magnetometro - Google Patents

Metodo de determinacion del angulo de ruta por medio de un magnetometro de tres ejes montado fijamente en un avion y de calibracion automatica de dicho magnetometro

Info

Publication number
ES2002936A6
ES2002936A6 ES8603476A ES8603476A ES2002936A6 ES 2002936 A6 ES2002936 A6 ES 2002936A6 ES 8603476 A ES8603476 A ES 8603476A ES 8603476 A ES8603476 A ES 8603476A ES 2002936 A6 ES2002936 A6 ES 2002936A6
Authority
ES
Spain
Prior art keywords
aircraft
automatically calibrating
axis magnetometer
flight
rigidly fitted
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
ES8603476A
Other languages
English (en)
Inventor
Manfred Baumker
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Litef GmbH
Original Assignee
Litef GmbH
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 Litef GmbH filed Critical Litef GmbH
Publication of ES2002936A6 publication Critical patent/ES2002936A6/es
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
    • G01C17/38Testing, calibrating, or compensating of compasses

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Measuring Magnetic Variables (AREA)

Abstract

EL METODO DE DETERMINACION DEL ANGULO DE RUTA POR MEDIO DE UN MAGNETOMETRO DE TRES EJES MONTADOS FIJAMENTE EN UN AVION Y DE CALIBRACION AUTOMATICA DE LA EXACTITUD DE RUMBO, QUE SE NECESITA A INTERVALOS ESPECIFICOS DE TIEMPO A CAUSA DE CAMPOS MAGNETICOS INTEREFERENTES EN EL VEHICULO Y DE ERRORES CAUSADOS POR LOS INTRUMENTOS, SE REALIZA EN VUELO Y COMPENSA LAS FUENTES PRINCIPALES DE ERROR DEL MAGNETOMETRO. EL VUELO DE CALIBRACION DEBE INCLUIR MANIOBRAS ESPECIFICAS DE VUELO (SIN CAMBIAR DE POSICION). EL METODO RESULTA ESPECIALMENTE ADECUADO PARA HELICOPTEROS DOTADOS DE MAGNETOMETROS DE TRES EJES.
ES8603476A 1985-12-20 1986-12-18 Metodo de determinacion del angulo de ruta por medio de un magnetometro de tres ejes montado fijamente en un avion y de calibracion automatica de dicho magnetometro Expired ES2002936A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP85116345A EP0226653B1 (de) 1985-12-20 1985-12-20 Verfahren zur Kurswinkelbestimmung mittels und zur automatischen Kalibration eines in einem Luftfahrzeug fest montierten Dreiachsen-Magnetometers

Publications (1)

Publication Number Publication Date
ES2002936A6 true ES2002936A6 (es) 1988-10-01

Family

ID=8193956

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8603476A Expired ES2002936A6 (es) 1985-12-20 1986-12-18 Metodo de determinacion del angulo de ruta por medio de un magnetometro de tres ejes montado fijamente en un avion y de calibracion automatica de dicho magnetometro

Country Status (5)

Country Link
US (1) US4870602A (es)
EP (1) EP0226653B1 (es)
JP (1) JPS62157518A (es)
DE (1) DE3568374D1 (es)
ES (1) ES2002936A6 (es)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4843865A (en) * 1988-02-29 1989-07-04 Digicourse, Inc. Method of calibrating a compass heading
JPH02120613A (ja) * 1988-10-28 1990-05-08 Japan Aviation Electron Ind Ltd 方位計
JPH07101174B2 (ja) * 1989-01-06 1995-11-01 日産自動車株式会社 車両用方位計
JPH07117415B2 (ja) * 1989-07-17 1995-12-18 日産自動車株式会社 車両用方位計
JP2514254B2 (ja) * 1989-08-11 1996-07-10 日産自動車株式会社 車両用方位計
US5297065A (en) * 1991-12-27 1994-03-22 Chrysler Corporation Magnetic transient detection and calibration technique for an auto-calibrating compass
DE4439945C1 (de) * 1994-11-09 1996-02-08 Leica Ag Verfahren zur Stabilisierung der Richtungsanzeige von Magnetkompassen
FR2728338A1 (fr) * 1994-12-19 1996-06-21 Eurocopter France Procede et dispositif d'identification simultanee et de correction des erreurs dues a des perturbations magnetiques et a de mauvais alignements dans les mesures d'un magnetometre
FR2732773B1 (fr) * 1995-04-10 1997-06-06 Eurocopter France Procede et dispositif d'identification simultanee et de correction d'erreurs dans les mesures d'un magnetometre
RU2098764C1 (ru) * 1996-05-29 1997-12-10 Русланов Александр Семенович Способ определения местоположения подвижных объектов и устройство для его реализации
IT1299404B1 (it) * 1998-04-01 2000-03-16 Finmeccanica Spa Sistema di sensori inerziali e magnetici atto a determinare l'angolo di orientamento rispetto al nord geografico
JP2006176084A (ja) * 2004-12-24 2006-07-06 Advics:Kk 車両挙動センサの検出値補正方法
KR100666160B1 (ko) 2004-12-29 2007-01-09 한국항공우주연구원 궤도기하학을 이용한 인공위성 자기센서의 바이어스보정방법
US7219033B2 (en) * 2005-02-15 2007-05-15 Magneto Inertial Sensing Technology, Inc. Single/multiple axes six degrees of freedom (6 DOF) inertial motion capture system with initial orientation determination capability
US7275008B2 (en) * 2005-09-02 2007-09-25 Nokia Corporation Calibration of 3D field sensors
KR20080026395A (ko) * 2006-09-20 2008-03-25 삼성전자주식회사 자기 환경을 고려한 컴퍼스 센서의 교정 방법 및 장치와이를 이용한 방위각 측정 방법 및 장치
FR2931248B1 (fr) * 2008-05-14 2012-07-27 Movea Sa Systeme de mesure de champ magnetique comprenant un capteur triaxial de mesure de champ magnetique mobile conjointement avec un element porteur perturbant les mesures et procede associe
US9157747B2 (en) * 2013-03-15 2015-10-13 Innovative Solutions And Support, Inc. Method of calibrating a heading reference system
US9476734B2 (en) * 2013-03-15 2016-10-25 Innovative Solutions And Support, Inc. Systems and methods for calibrating and adjusting a heading reference system
CN104165642B (zh) * 2014-08-29 2017-02-15 东南大学 一种用于导航***航向角直接校正补偿方法
FR3029642B1 (fr) * 2014-12-09 2017-12-08 ISKn Procede de localisation d'au moins un objet magnetique mobile, et systeme associe
US10365296B2 (en) 2016-09-29 2019-07-30 Innovative Solutions & Support, Inc. Systems and methods for compensating for the absence of a sensor measurement in a heading reference system
US10921153B2 (en) 2018-10-05 2021-02-16 Honeywell International In. System and method to construct a magnetic calibration (MAG-CAL) pattern for depicting the progress of a calibration of a magnetometer of an aircraft displayed by a cockpit display
CN112213678B (zh) * 2020-10-27 2022-03-25 中国人民解放军海军工程大学 一种矢量磁探仪三轴数据校正与补偿方法
CN114485728A (zh) * 2022-01-04 2022-05-13 中国煤炭科工集团太原研究院有限公司 一种捷联惯导***现场快速自标定方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3728525A (en) * 1971-10-19 1973-04-17 Us Navy Magnetic navigation system
GB1601459A (en) * 1977-05-17 1981-10-28 Allen & Hanburys Ltd Aminoalkyl thiophene derivatives
US4321678A (en) * 1977-09-14 1982-03-23 Bodenseewerk Geratetechnik Gmbh Apparatus for the automatic determination of a vehicle position
AR228941A1 (es) * 1978-04-26 1983-05-13 Glaxo Group Ltd Procedimiento para preparar nuevos derivados de 3,5-diamino-1,2,4-triazol que son activos contra receptores histaminicos
US4347730A (en) * 1979-01-22 1982-09-07 The United States Of America As Represented By The Secretary Of The Army Method and apparatus for calibrating gyroscopically-stabilized, magnetically-slaved heading reference system
US4303978A (en) * 1980-04-18 1981-12-01 The Boeing Company Integrated-strapdown-air-data sensor system
FR2484079A1 (fr) * 1980-06-05 1981-12-11 Crouzet Sa Procede de compensation des perturbations magnetiques dans la determination d'un cap magnetique, et dispositif pour la mise en oeuvre de ce procede
US4394508A (en) * 1980-06-07 1983-07-19 Bristol-Myers Company Chemical compounds
US4390701A (en) * 1981-05-18 1983-06-28 Bristol-Myers Company 1-Amino-2-[3-(3-piperidinomethylphenoxy)propylamino]cyclobutene-3,4-dione
GB2128749B (en) * 1982-10-12 1987-04-15 Plessey Co Plc Electronic compass with tilt compensation
DE3422490A1 (de) * 1984-06-16 1985-12-19 Robert Bosch Gmbh, 7000 Stuttgart Verfahren zur korrektur von winkelfehlern bei einem elektronischen kompass in fahrzeugen

Also Published As

Publication number Publication date
JPS62157518A (ja) 1987-07-13
US4870602A (en) 1989-09-26
EP0226653A1 (de) 1987-07-01
DE3568374D1 (en) 1989-03-30
EP0226653B1 (de) 1989-02-22

Similar Documents

Publication Publication Date Title
ES2002936A6 (es) Metodo de determinacion del angulo de ruta por medio de un magnetometro de tres ejes montado fijamente en un avion y de calibracion automatica de dicho magnetometro
US4462165A (en) Three axis orientation sensor for an aircraft or the like
JPS5559352A (en) Magnetic source detecting method through measurement of magnetic field
EP0229468A3 (en) Magnetic flux detector correction system
GB899860A (en) Vertical velocity measuring system
US2887872A (en) Method of measuring and compensating for deviation errors for earth's field responsive instruments
Liu et al. Compass deviation analysis and compensation for a three-axis strapdown magnetic heading system
HUG High accuracy Doppler navigation employing optimum integrated position fix information
Zhang et al. Research on high precision intelligent digital magnetic heading system
DEVAUD Static, non-swinging arrangement for determining course on board a vehicle
HOTOP Flight tests for a strapdown system(MSS): The results of a special flight test
Downs A lab test to find the major error sources in a laser strapdown inertial navigator
CRENSHAW Airborne laboratory measurement of aircraft performance and stability and control for light aircraft. Supplement
KOEHLER Effect of installation and calibration errors of sensors on system identification results of an aircraft
Swanson A navigation monitor for VLF signals
KHARIN Flight testing of flight control and navigation equipment((Russian book))(Letnye ispytaniia sistem pilotazhno-navigatsionnogo oborudovaniia)
SUNTSEV Some applications of a generalized frequency method for the synthesis of linear systems with feedbacks(O nekotorykh prilozheniiakh obobshchennogo chastotnogo metoda sinteza lineinykh sistem s obratnymi sviaziami)
LAWRENCE Error model verification for a three axis laser gyro strapdown inertial measurement unit[M. S. Thesis]
MARCOS Application of satellite accelerometer data to improve density models[Environmental Research Papers]
RAKHTEENKO Gyroscopic orientation systems((Russian book))(Giroskopicheskie sistemy orientatsii)
SALWEN et al. Phase derived navigation studies(aircraft landing system with perspective display system to pilot)[Final Report, Nov. 1974- Sep. 1975]
ILIFF et al. The AFGL(Air Force Geophysics Laboratory) absolute gravity system's error budget revisted(Environmental Research Papers, Jan. 1984- May)(1985)
REED TSPI data processing in the telemetry environment((Time Space Position Information for flight tests))
SU1840368A1 (ru) Способ коррекции комплексной инс по аномалии гравитационного поля земли
SNELL A method of estimating aircraft attitude from fly by wire flight control system data