DE60100168D1 - Verfahren für die Ausrichtung einer Inertialmesseinheit in Anwesenheit unbekannter Flugzeugmessverzögerungen - Google Patents

Verfahren für die Ausrichtung einer Inertialmesseinheit in Anwesenheit unbekannter Flugzeugmessverzögerungen

Info

Publication number
DE60100168D1
DE60100168D1 DE60100168T DE60100168T DE60100168D1 DE 60100168 D1 DE60100168 D1 DE 60100168D1 DE 60100168 T DE60100168 T DE 60100168T DE 60100168 T DE60100168 T DE 60100168T DE 60100168 D1 DE60100168 D1 DE 60100168D1
Authority
DE
Germany
Prior art keywords
aligning
procedure
delays
vehicle
measurement unit
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 - Fee Related
Application number
DE60100168T
Other languages
English (en)
Other versions
DE60100168T2 (de
Inventor
Joseph Ben-Jaacov
Jacob Reiner
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.)
Rafael Advanced Defense Systems Ltd
Original Assignee
Rafael Advanced Defense Systems Ltd
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 Rafael Advanced Defense Systems Ltd filed Critical Rafael Advanced Defense Systems Ltd
Publication of DE60100168D1 publication Critical patent/DE60100168D1/de
Application granted granted Critical
Publication of DE60100168T2 publication Critical patent/DE60100168T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Image Analysis (AREA)
  • Traffic Control Systems (AREA)
DE60100168T 2000-06-05 2001-06-05 Verfahren für die Ausrichtung einer Inertialmesseinheit in Anwesenheit unbekannter Flugzeugmessverzögerungen Expired - Fee Related DE60100168T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL13656600 2000-06-05
IL136566A IL136566A (en) 2000-06-05 2000-06-05 Method for adjusting an inertial measurement unit in the presence of delays in unknown aircraft measurements

Publications (2)

Publication Number Publication Date
DE60100168D1 true DE60100168D1 (de) 2003-05-15
DE60100168T2 DE60100168T2 (de) 2004-02-26

Family

ID=11074223

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60100168T Expired - Fee Related DE60100168T2 (de) 2000-06-05 2001-06-05 Verfahren für die Ausrichtung einer Inertialmesseinheit in Anwesenheit unbekannter Flugzeugmessverzögerungen

Country Status (6)

Country Link
US (1) US6556895B2 (de)
EP (1) EP1162431B1 (de)
AT (1) ATE237123T1 (de)
DE (1) DE60100168T2 (de)
ES (1) ES2194811T3 (de)
IL (1) IL136566A (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002035183A1 (en) * 2000-07-28 2002-05-02 Litton Systems, Inc. Attitude alignment of a slave inertial measurement system
FR2878954B1 (fr) * 2004-12-07 2007-03-30 Sagem Systeme de navigation inertielle hybride base sur un modele cinematique
US20070088496A1 (en) * 2005-07-20 2007-04-19 Atair Aerospace, Inc. Automatic heading and reference system
CN101634612B (zh) * 2009-08-21 2011-01-05 北京航空航天大学 一种无人机久航飞行参数确定方法
US8515672B1 (en) * 2012-03-01 2013-08-20 Honeywell International Inc. Systems and methods to incorporate master navigation system resets during transfer alignment
CN104655132B (zh) * 2015-02-11 2017-08-25 北京航空航天大学 一种基于加速度计的机体弹性变形角估计方法
CN106441301A (zh) * 2016-09-19 2017-02-22 北京机械设备研究所 一种飞行器发射初始参数获取方法及系统
CN106595711A (zh) * 2016-12-21 2017-04-26 东南大学 一种基于递推四元数的捷联惯性导航系统粗对准方法
US11199410B2 (en) 2019-04-30 2021-12-14 Stmicroelectronics, Inc. Dead reckoning by determining misalignment angle between movement direction and sensor heading direction
US11747142B2 (en) 2019-04-30 2023-09-05 Stmicroelectronics, Inc. Inertial navigation system capable of dead reckoning in vehicles
CN112229271B (zh) * 2020-09-23 2022-08-30 郑州天一飞控机电有限公司 一种直升机载导弹传递对准延时时间估计方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4288049A (en) * 1971-01-19 1981-09-08 The United States Of America As Represented By The Secretary Of The Navy Remote targeting system for guided missiles
US5245909A (en) * 1990-05-07 1993-09-21 Mcdonnell Douglas Corporation Automatic sensor alignment
FR2668447B1 (fr) * 1990-10-29 1993-01-22 Aerospatiale Systeme pour l'alignement de la centrale inertielle d'un vehicule porte sur celle d'un vehicule porteur.
US5260709A (en) * 1991-12-19 1993-11-09 Hughes Aircraft Company Autonomous precision weapon delivery using synthetic array radar
US5470033A (en) * 1994-07-28 1995-11-28 Tsai; Yeong-Shyeong Method for controlling a carrier which is used to carry a flight vehicle
US5672872A (en) * 1996-03-19 1997-09-30 Hughes Electronics FLIR boresight alignment
US6278945B1 (en) * 1997-11-24 2001-08-21 American Gnc Corporation Fully-coupled positioning process and system thereof
US6094163A (en) * 1998-01-21 2000-07-25 Min-I James Chang Ins alignment method using a doppler sensor and a GPS/HVINS

Also Published As

Publication number Publication date
ES2194811T3 (es) 2003-12-01
IL136566A (en) 2007-07-24
US6556895B2 (en) 2003-04-29
IL136566A0 (en) 2003-06-24
EP1162431A1 (de) 2001-12-12
EP1162431B1 (de) 2003-04-09
ATE237123T1 (de) 2003-04-15
DE60100168T2 (de) 2004-02-26
US20020049519A1 (en) 2002-04-25

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Legal Events

Date Code Title Description
8332 No legal effect for de
8370 Indication related to discontinuation of the patent is to be deleted
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee