ES2055977T3 - Sistema para la alineacion de la central inercial de un vehiculo transportado con la del un vehiculo transportador. - Google Patents

Sistema para la alineacion de la central inercial de un vehiculo transportado con la del un vehiculo transportador.

Info

Publication number
ES2055977T3
ES2055977T3 ES91402820T ES91402820T ES2055977T3 ES 2055977 T3 ES2055977 T3 ES 2055977T3 ES 91402820 T ES91402820 T ES 91402820T ES 91402820 T ES91402820 T ES 91402820T ES 2055977 T3 ES2055977 T3 ES 2055977T3
Authority
ES
Spain
Prior art keywords
vehicle
inertia
alignment
power plant
carrier
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 - Lifetime
Application number
ES91402820T
Other languages
English (en)
Inventor
Pierre Gaide
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2055977T3 publication Critical patent/ES2055977T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/007—Preparatory measures taken before the launching of the guided missiles
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

SISTEMA QUE PERMITE, POR EJEMPLO, LA INICIALIZACION DE LA CENTRAL DE INERCIA (CNM) DE UN MISIL A PARTIR DE LA CENTRAL DE INERCIA (CNP) DEL PORTADOR DE ESTE MISIL. -SEGUN LA INVENCION, SE PREVE UN DISPOSITIVO DE CONTROL (A) DE LA INFORMACION DE LA CENTRAL DE INERCIA DEL PORTADOR (CNP) EN LA CENTRAL DE INERCIA (CNM) DEL MISIL Y UN FILTRO DE KALMAN (K) MONTADO EN PARALELO SOBRE DICHO REVESTIMIENTO DE CONTROL (A) Y DESTINADO A IDENTIFICAR LOS ERRORES DE ARMONIZACION ENTRE LAS DOS CENTRALES DE INERCIA.
ES91402820T 1990-10-29 1991-10-23 Sistema para la alineacion de la central inercial de un vehiculo transportado con la del un vehiculo transportador. Expired - Lifetime ES2055977T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9013386A FR2668447B1 (fr) 1990-10-29 1990-10-29 Systeme pour l'alignement de la centrale inertielle d'un vehicule porte sur celle d'un vehicule porteur.

Publications (1)

Publication Number Publication Date
ES2055977T3 true ES2055977T3 (es) 1994-09-01

Family

ID=9401660

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91402820T Expired - Lifetime ES2055977T3 (es) 1990-10-29 1991-10-23 Sistema para la alineacion de la central inercial de un vehiculo transportado con la del un vehiculo transportador.

Country Status (7)

Country Link
US (1) US5150856A (es)
EP (1) EP0484202B1 (es)
JP (1) JPH04265817A (es)
CA (1) CA2054377A1 (es)
DE (1) DE69102048T2 (es)
ES (1) ES2055977T3 (es)
FR (1) FR2668447B1 (es)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5281901A (en) * 1990-12-03 1994-01-25 Eaton-Kenway, Inc. Downward compatible AGV system and methods
FR2673711B1 (fr) * 1991-03-07 1995-09-15 Aerospatiale Procede et systeme d'harmonisation autonome d'equipements a bord d'un vehicule, utilisant des moyens de mesure du champ de gravite terrestre.
FR2673712B1 (fr) * 1991-03-07 1993-06-18 Aerospatiale Procede et systeme d'harmonisation autonome d'equipements a bord d'un vehicule, utilisant des moyens de mesure des champs de gravite et magnetique terrestres.
US5442560A (en) * 1993-07-29 1995-08-15 Honeywell, Inc. Integrated guidance system and method for providing guidance to a projectile on a trajectory
US5948045A (en) * 1995-05-23 1999-09-07 State Of Israel-Ministry Of Defense Armament Development Authority-Rafael Method for airbourne transfer alignment of an inertial measurement unit
IL136566A (en) * 2000-06-05 2007-07-24 Rafael Advanced Defense Sys Method for adjusting an inertial measurement unit in the presence of delays in unknown aircraft measurements
US6380526B1 (en) * 2000-08-23 2002-04-30 Honeywell International Inc. Employing booster trajectory in a payload inertial measurement unit
FR2824132B1 (fr) * 2001-04-27 2007-07-13 France Etat Dispositif, et procede associe, apte a determiner la direction d'une cible
US7509216B2 (en) * 2004-03-29 2009-03-24 Northrop Grumman Corporation Inertial navigation system error correction
FR2869997B1 (fr) * 2004-05-04 2006-06-23 Commissariat Energie Atomique Accelerometre en boucle fermee avec detection d'erreur
CA2565143C (en) * 2004-05-12 2014-07-08 Northrop Grumman Corporation System and method for aligning multiple navigation components
WO2006083267A2 (en) 2004-05-13 2006-08-10 Northrop Grumman Corporation System for interferometric sensing
DE102006029148B4 (de) * 2006-06-24 2010-08-05 Lfk-Lenkflugkörpersysteme Gmbh Verfahren zur Überprüfung einer inertialen Messeinheit von Fahrzeugen, insbesondere von Luftfahrzeugen, im stationären Zustand
FR2924215B1 (fr) * 2007-11-23 2010-01-01 Thales Sa Systeme comprenant deux instruments combines et procede d'alignement du systeme
JP5145371B2 (ja) * 2010-04-08 2013-02-13 日本航空電子工業株式会社 慣性航法装置
WO2012005786A2 (en) * 2010-04-09 2012-01-12 Bae Systems Information And Electronic Systems Integration Inc. Automatic re-initialization of resonant sensors in rocket and missile guidance systems
US8812233B2 (en) * 2011-12-27 2014-08-19 Caterpillar Inc. Error detection for inertial measurement units
FR3003639B1 (fr) * 2013-03-20 2015-04-10 Mbda France Procede et dispositif pour ameliorer la navigation inertielle d'un engin.
DE102013218043B4 (de) * 2013-09-10 2024-06-20 Continental Automotive Technologies GmbH Verfahren zum Bereitstellen relativer Messdaten für einen Fusionssensor
US10901095B2 (en) 2014-04-25 2021-01-26 Nec Corporation Position and attitude estimation device, image processing device, and position and attitude estimation method
US10503245B2 (en) 2016-09-21 2019-12-10 Apple Inc. Relative intertial measurement system
FR3065067B1 (fr) 2017-04-07 2020-02-28 Airbus Helicopters Systeme et procede d'analyse et de surveillance des mouvements parasites d'une centrale inertielle pendant une phase d'alignement statique.
CN110132269A (zh) * 2019-06-10 2019-08-16 西北工业大学 一种导弹高精度垂直发射初始姿态获取方法
CN117533513A (zh) * 2023-04-14 2024-02-09 中国人民解放军国防科技大学 一种电磁弹射飞行器的在线测速反馈控制方法和系统
CN120232447A (zh) * 2023-12-29 2025-07-01 优奈柯恩(北京)科技有限公司 用于状态估计的方法、装置、电子设备及存储介质

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE276663C (es) *
DE179197C (es) *
DE184632C (es) *
US4032759A (en) * 1975-10-24 1977-06-28 The Singer Company Shipboard reference for an aircraft navigation system
US4444086A (en) * 1981-12-23 1984-04-24 The United States Of America As Represented By The Secretary Of The Army Missile azimuth aiming apparatus
US4495850A (en) * 1982-08-26 1985-01-29 The United States Of America As Represented By The Secretary Of The Army Azimuth transfer scheme for a strapdown Inertial Measurement Unit
DE3438719A1 (de) * 1984-10-23 1986-04-24 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Anordnung zur gegenseitigen lagebestimmung von mutter- und tochter-traegheitsnavigationssystemen
DE3445463A1 (de) * 1984-12-13 1986-06-19 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Anordnung zur initialisierung und/oder rekalibrierung eines tochter-traegheitsnavigationssystems
DE3701583A1 (de) * 1987-01-21 1988-08-04 Bodenseewerk Geraetetech Einrichtung zur bestimmung der zeitlich veraenderlichen lage und von fehlern eines tochternavigationssystems relativ zu einem mutternavigationssystem

Also Published As

Publication number Publication date
EP0484202A1 (fr) 1992-05-06
FR2668447A1 (fr) 1992-04-30
EP0484202B1 (fr) 1994-05-18
US5150856A (en) 1992-09-29
DE69102048D1 (de) 1994-06-23
DE69102048T2 (de) 1994-09-01
FR2668447B1 (fr) 1993-01-22
CA2054377A1 (fr) 1992-04-30
JPH04265817A (ja) 1992-09-22

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