IL153898A0 - Attitude alignment of a slave inertial measurement system - Google Patents

Attitude alignment of a slave inertial measurement system

Info

Publication number
IL153898A0
IL153898A0 IL15389801A IL15389801A IL153898A0 IL 153898 A0 IL153898 A0 IL 153898A0 IL 15389801 A IL15389801 A IL 15389801A IL 15389801 A IL15389801 A IL 15389801A IL 153898 A0 IL153898 A0 IL 153898A0
Authority
IL
Israel
Prior art keywords
measurement system
inertial measurement
attitude alignment
slave inertial
slave
Prior art date
Application number
IL15389801A
Other languages
English (en)
Original Assignee
Litton Systems 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 Litton Systems Inc filed Critical Litton Systems Inc
Publication of IL153898A0 publication Critical patent/IL153898A0/xx

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
    • G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles

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)
  • Aviation & Aerospace Engineering (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
IL15389801A 2000-07-28 2001-07-27 Attitude alignment of a slave inertial measurement system IL153898A0 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US22131500P 2000-07-28 2000-07-28
PCT/US2001/023659 WO2002035183A1 (en) 2000-07-28 2001-07-27 Attitude alignment of a slave inertial measurement system

Publications (1)

Publication Number Publication Date
IL153898A0 true IL153898A0 (en) 2003-07-31

Family

ID=22827289

Family Applications (1)

Application Number Title Priority Date Filing Date
IL15389801A IL153898A0 (en) 2000-07-28 2001-07-27 Attitude alignment of a slave inertial measurement system

Country Status (5)

Country Link
US (1) US7133776B2 (xx)
EP (1) EP1328775A1 (xx)
JP (1) JP3850796B2 (xx)
IL (1) IL153898A0 (xx)
WO (1) WO2002035183A1 (xx)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1371931B1 (de) 2002-06-14 2006-08-23 Oerlikon Contraves Ag Verfahren und Vorrichtung zur Bestimmung eines Winkelfehlers und Verwendung der Vorrichtung
US8224574B2 (en) * 2004-05-12 2012-07-17 Northrop Grumman Guidance And Electronics Company, Inc. System for multiple navigation components
CA2565165A1 (en) * 2004-05-13 2006-08-10 Northrop Grumman Corporation System for interferometric sensing
US8209068B2 (en) * 2004-06-02 2012-06-26 Rockwell Collins Control Technologies, Inc. Systems and methods for controlling dynamic systems
US7206694B2 (en) * 2004-07-16 2007-04-17 Northrop Grumman Corporation Transfer alignment of navigation systems
WO2006104552A1 (en) 2005-03-29 2006-10-05 Honeywell International Inc. Method and apparatus for high accuracy relative motion determinatation using inertial sensors
US8019538B2 (en) 2007-07-25 2011-09-13 Honeywell International Inc. System and method for high accuracy relative navigation
US8558153B2 (en) * 2009-01-23 2013-10-15 Raytheon Company Projectile with inertial sensors oriented for enhanced failure detection
US20100318257A1 (en) * 2009-06-15 2010-12-16 Deep Kalinadhabhotla Method and system for automatically calibrating a three-axis accelerometer device
US8566055B1 (en) * 2010-02-12 2013-10-22 Lockheed Martin Corporation Gyro indexing compensation method and system
US8666694B2 (en) 2011-08-12 2014-03-04 Honeywell International Inc. Estimation of an initial condition inertial reference frame
US8543266B2 (en) * 2011-10-03 2013-09-24 The Boeing Company Modified Kalman filter for generation of attitude error corrections
FR3000219B1 (fr) * 2012-12-26 2015-01-09 Sagem Defense Securite Procede de comparaison de deux centrales inertielles solidaires d'un meme porteur
CN103885455B (zh) * 2014-03-25 2015-03-25 许凯华 跟踪测量机器人
JP6080189B2 (ja) * 2014-08-15 2017-02-15 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ インラインセンサの較正方法及び較正装置
US20170307334A1 (en) * 2016-04-26 2017-10-26 Martin William Greenwood Apparatus and System to Counter Drones Using a Shoulder-Launched Aerodynamically Guided Missile
CN106502259A (zh) * 2016-11-21 2017-03-15 国网山东省电力公司电力科学研究院 电力巡检用小型光电吊舱控制装置、吊舱、无人机及方法
US10989539B1 (en) * 2018-04-25 2021-04-27 Bae Systems Information And Electronic Systems Integration Inc. Alignment of electrical devices using inertial measurement units
FR3081220B1 (fr) * 2018-05-16 2020-05-29 Safran Electronics & Defense Procede d'harmonisation de deux unites de mesure inertielle l'une avec l'autre et systeme de navigation mettant en œuvre ce procede
CN109141476B (zh) * 2018-09-27 2019-11-08 东南大学 一种动态变形下传递对准过程中角速度解耦合方法
FR3088715B1 (fr) * 2018-11-20 2020-11-27 Safran Electronics & Defense Dispositif de mesure inertielle
CN110243362B (zh) * 2019-06-27 2023-03-21 西北工业大学 一种中高空超声速靶标导航方法
DE102019217448A1 (de) * 2019-11-12 2021-05-12 Robert Bosch Gmbh Verfahren und und Vorrichtung zum Erstellen eines Kalibrierwertes zum Kalibrieren einer inertialen Messeinheit für ein Fahrzeug
CN112649884B (zh) * 2021-01-13 2024-02-09 中国自然资源航空物探遥感中心 应用于航空电磁测量系统的吊舱姿态实时调整方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3056290A (en) * 1959-12-31 1962-10-02 Kearfott Company Inc Multi-vehicular azimuth alignment computer
US3803387A (en) * 1972-09-20 1974-04-09 Us Navy Alignment error detection system
DE3812783A1 (de) * 1988-04-16 1989-10-26 Messerschmitt Boelkow Blohm Verfahren und einrichtung zur automatischen azimutausrichtung der inertialnavigation
JPH02128696A (ja) 1988-11-09 1990-05-17 Teijin Ltd 新規生理活性ポリペプチド
AU5245096A (en) * 1995-05-23 1996-12-05 State of Israel-Ministry of Defence, Armament Deve lopment Authority-Rafael A method for airbourne transfer alignment of an inertial measurement unit
US5672872A (en) * 1996-03-19 1997-09-30 Hughes Electronics FLIR boresight alignment
JP3939786B2 (ja) 1996-09-19 2007-07-04 東北リコー株式会社 孔版印刷装置
US6061611A (en) * 1998-01-06 2000-05-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Closed-form integrator for the quaternion (euler angle) kinematics equations
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
US7606665B2 (en) * 2003-08-29 2009-10-20 Honeywell International Inc. System and method for employing an aided-alignment mode to align an inertial reference system
US7206694B2 (en) * 2004-07-16 2007-04-17 Northrop Grumman Corporation Transfer alignment of navigation systems

Also Published As

Publication number Publication date
JP3850796B2 (ja) 2006-11-29
WO2002035183A1 (en) 2002-05-02
JP2004512517A (ja) 2004-04-22
US7133776B2 (en) 2006-11-07
US20040030464A1 (en) 2004-02-12
EP1328775A1 (en) 2003-07-23

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