Improved accelerometer and magnetometer-based solution to solve quaternion
Light overloaded small aircraft, such as ducted fan MAV, could use accelerometer and magnetometer to measure acceleration and earth magnetic field in the body coordinate frame. There is a quaternion that relates the measured accelerations and earth magnetic field in the body coordinate frame to calc...
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creator | Feng Zhou Yanxuan Wu Ningjun Fan |
description | Light overloaded small aircraft, such as ducted fan MAV, could use accelerometer and magnetometer to measure acceleration and earth magnetic field in the body coordinate frame. There is a quaternion that relates the measured accelerations and earth magnetic field in the body coordinate frame to calculated values in the earth coordinate frame. An overdetermined nonlinear equations which could get the quaternion need to be solved. So far, the Gauss-Newton iteration algorithm was being used most commonly to solve the overdetermined equations. However, when the inverse of Jacobian matrix is singular or conditioned, the iteration would be diverge. To overcome the problem, first, transferring the overdetermined problem to determined one by a premultiply transposition of Jacobian matrix, then using Correctional Newton with Parameter iteration algorithm to solve the determined equations. Compared to Gauss-Newton iteration algorithm, this method not only could converge more fast, but also could overcome the situation which Jacobian matrix is singular or conditioned. |
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There is a quaternion that relates the measured accelerations and earth magnetic field in the body coordinate frame to calculated values in the earth coordinate frame. An overdetermined nonlinear equations which could get the quaternion need to be solved. So far, the Gauss-Newton iteration algorithm was being used most commonly to solve the overdetermined equations. However, when the inverse of Jacobian matrix is singular or conditioned, the iteration would be diverge. To overcome the problem, first, transferring the overdetermined problem to determined one by a premultiply transposition of Jacobian matrix, then using Correctional Newton with Parameter iteration algorithm to solve the determined equations. Compared to Gauss-Newton iteration algorithm, this method not only could converge more fast, but also could overcome the situation which Jacobian matrix is singular or conditioned.</description><identifier>ISBN: 9781467322478</identifier><identifier>ISBN: 1467322474</identifier><identifier>EISBN: 8993215049</identifier><identifier>EISBN: 9788993215045</identifier><language>eng</language><publisher>IEEE</publisher><subject>attitude estimation ; Correctional Newton ; Correctional Newton with Parameter ; Earth ; Jacobian matrices ; Magnetic field measurement ; Magnetometers ; Mathematical model ; Nonlinear equations ; quaternion ; Quaternions</subject><ispartof>2012 12th International Conference on Control, Automation and Systems, 2012, p.2093-2096</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/6393231$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2051,54898</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/6393231$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Feng Zhou</creatorcontrib><creatorcontrib>Yanxuan Wu</creatorcontrib><creatorcontrib>Ningjun Fan</creatorcontrib><title>Improved accelerometer and magnetometer-based solution to solve quaternion</title><title>2012 12th International Conference on Control, Automation and Systems</title><addtitle>ICCAS</addtitle><description>Light overloaded small aircraft, such as ducted fan MAV, could use accelerometer and magnetometer to measure acceleration and earth magnetic field in the body coordinate frame. There is a quaternion that relates the measured accelerations and earth magnetic field in the body coordinate frame to calculated values in the earth coordinate frame. An overdetermined nonlinear equations which could get the quaternion need to be solved. So far, the Gauss-Newton iteration algorithm was being used most commonly to solve the overdetermined equations. However, when the inverse of Jacobian matrix is singular or conditioned, the iteration would be diverge. To overcome the problem, first, transferring the overdetermined problem to determined one by a premultiply transposition of Jacobian matrix, then using Correctional Newton with Parameter iteration algorithm to solve the determined equations. Compared to Gauss-Newton iteration algorithm, this method not only could converge more fast, but also could overcome the situation which Jacobian matrix is singular or conditioned.</description><subject>attitude estimation</subject><subject>Correctional Newton</subject><subject>Correctional Newton with Parameter</subject><subject>Earth</subject><subject>Jacobian matrices</subject><subject>Magnetic field measurement</subject><subject>Magnetometers</subject><subject>Mathematical model</subject><subject>Nonlinear equations</subject><subject>quaternion</subject><subject>Quaternions</subject><isbn>9781467322478</isbn><isbn>1467322474</isbn><isbn>8993215049</isbn><isbn>9788993215045</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2012</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNotT8lqAzEUcymBtul8QS_-gQFv4-VYQpeUQC-5hzf2c5gyS2o7gf59XdKThCSEdEMerHNS8I4pd0saZyxX2kghlLF3pMn5izHGOdOW2XvysZ1OablgoOA9jpiWCQsmCnOgExxnLFeh7SHXUF7GcxmWmZblj1-Qfp-h2nPVHskqwpix-cc12b--7Dfv7e7zbbt53rWDY6W1vTCdxzrKcHAYFGdCQFBOYuS-rlVCKwMx-g45KM0Row0BgpPa9R7lmjxdawdEPJzSMEH6OWhZP0sufwEXDUog</recordid><startdate>201210</startdate><enddate>201210</enddate><creator>Feng Zhou</creator><creator>Yanxuan Wu</creator><creator>Ningjun Fan</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201210</creationdate><title>Improved accelerometer and magnetometer-based solution to solve quaternion</title><author>Feng Zhou ; Yanxuan Wu ; Ningjun Fan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i90t-8b275ce81471a9ed41022ad493ef1c97842647affc5e1a461eef8ddad9369bce3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2012</creationdate><topic>attitude estimation</topic><topic>Correctional Newton</topic><topic>Correctional Newton with Parameter</topic><topic>Earth</topic><topic>Jacobian matrices</topic><topic>Magnetic field measurement</topic><topic>Magnetometers</topic><topic>Mathematical model</topic><topic>Nonlinear equations</topic><topic>quaternion</topic><topic>Quaternions</topic><toplevel>online_resources</toplevel><creatorcontrib>Feng Zhou</creatorcontrib><creatorcontrib>Yanxuan Wu</creatorcontrib><creatorcontrib>Ningjun Fan</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Feng Zhou</au><au>Yanxuan Wu</au><au>Ningjun Fan</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Improved accelerometer and magnetometer-based solution to solve quaternion</atitle><btitle>2012 12th International Conference on Control, Automation and Systems</btitle><stitle>ICCAS</stitle><date>2012-10</date><risdate>2012</risdate><spage>2093</spage><epage>2096</epage><pages>2093-2096</pages><isbn>9781467322478</isbn><isbn>1467322474</isbn><eisbn>8993215049</eisbn><eisbn>9788993215045</eisbn><abstract>Light overloaded small aircraft, such as ducted fan MAV, could use accelerometer and magnetometer to measure acceleration and earth magnetic field in the body coordinate frame. There is a quaternion that relates the measured accelerations and earth magnetic field in the body coordinate frame to calculated values in the earth coordinate frame. An overdetermined nonlinear equations which could get the quaternion need to be solved. So far, the Gauss-Newton iteration algorithm was being used most commonly to solve the overdetermined equations. However, when the inverse of Jacobian matrix is singular or conditioned, the iteration would be diverge. To overcome the problem, first, transferring the overdetermined problem to determined one by a premultiply transposition of Jacobian matrix, then using Correctional Newton with Parameter iteration algorithm to solve the determined equations. Compared to Gauss-Newton iteration algorithm, this method not only could converge more fast, but also could overcome the situation which Jacobian matrix is singular or conditioned.</abstract><pub>IEEE</pub><tpages>4</tpages></addata></record> |
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subjects | attitude estimation Correctional Newton Correctional Newton with Parameter Earth Jacobian matrices Magnetic field measurement Magnetometers Mathematical model Nonlinear equations quaternion Quaternions |
title | Improved accelerometer and magnetometer-based solution to solve quaternion |
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