Angular rate input attitude algorithm structure and parameter optimization method

Angular rate input attitude algorithm structure and parameter optimization method

The invention discloses a novel angular rate input attitude algorithm structure and a parameter optimization method. Aiming at the problem that the traditional angular rate input attitude algorithm coning error compensation structure cannot fully utilize available angular rate information, the inven...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: TANG CHUANYE, LV CAIPING, FANG LIN, SONG RUI, CHEN XIYUAN, HUANG HAOQIAN, HE KUNPENG
Format: Patent
Sprache:chi ; eng
Schlagworte:
GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator TANG CHUANYE
LV CAIPING
FANG LIN
SONG RUI
CHEN XIYUAN
HUANG HAOQIAN
HE KUNPENG
description The invention discloses a novel angular rate input attitude algorithm structure and a parameter optimization method. Aiming at the problem that the traditional angular rate input attitude algorithm coning error compensation structure cannot fully utilize available angular rate information, the invention provides an improved attitude algorithm coning error compensation structure so as to provide a novel angular rate input attitude algorithm structure. On the basis of defining the classical conical motion form and analyzing several necessary conical motion characteristics, the provided attitude algorithm coning error compensation structure is simplified to obtain a condensed attitude algorithm coning error compensation structure; a coning error compensation error criterion is defined, and the specific description of the error criterion is derived; a coning error compensation optimization object and a coning error compensation optimization method are selected, and parameter optimization designing on the coning e
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN103630135A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN103630135A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN103630135A3</originalsourceid><addsrcrecordid>eNqNyj0KwkAQhuE0FqLeYTyAkLBoH4JiJQj2YciOycL-Mftt4-lN4QGsXnh4t82zj3P1rKQMIRdzBTHgUK0Q-zmpwxKoQOuEqqtFS5mVg0CUUoYL7sNwKdJKS7L7ZvNmX-Tw66453q6v4X6SnEYpmSeJgnF4dK25mLYz597883wBT_s4og</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Angular rate input attitude algorithm structure and parameter optimization method</title><source>esp@cenet</source><creator>TANG CHUANYE ; LV CAIPING ; FANG LIN ; SONG RUI ; CHEN XIYUAN ; HUANG HAOQIAN ; HE KUNPENG</creator><creatorcontrib>TANG CHUANYE ; LV CAIPING ; FANG LIN ; SONG RUI ; CHEN XIYUAN ; HUANG HAOQIAN ; HE KUNPENG</creatorcontrib><description>The invention discloses a novel angular rate input attitude algorithm structure and a parameter optimization method. Aiming at the problem that the traditional angular rate input attitude algorithm coning error compensation structure cannot fully utilize available angular rate information, the invention provides an improved attitude algorithm coning error compensation structure so as to provide a novel angular rate input attitude algorithm structure. On the basis of defining the classical conical motion form and analyzing several necessary conical motion characteristics, the provided attitude algorithm coning error compensation structure is simplified to obtain a condensed attitude algorithm coning error compensation structure; a coning error compensation error criterion is defined, and the specific description of the error criterion is derived; a coning error compensation optimization object and a coning error compensation optimization method are selected, and parameter optimization designing on the coning e</description><language>chi ; eng</language><subject>GYROSCOPIC INSTRUMENTS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SURVEYING ; TESTING</subject><creationdate>2014</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140312&amp;DB=EPODOC&amp;CC=CN&amp;NR=103630135A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140312&amp;DB=EPODOC&amp;CC=CN&amp;NR=103630135A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TANG CHUANYE</creatorcontrib><creatorcontrib>LV CAIPING</creatorcontrib><creatorcontrib>FANG LIN</creatorcontrib><creatorcontrib>SONG RUI</creatorcontrib><creatorcontrib>CHEN XIYUAN</creatorcontrib><creatorcontrib>HUANG HAOQIAN</creatorcontrib><creatorcontrib>HE KUNPENG</creatorcontrib><title>Angular rate input attitude algorithm structure and parameter optimization method</title><description>The invention discloses a novel angular rate input attitude algorithm structure and a parameter optimization method. Aiming at the problem that the traditional angular rate input attitude algorithm coning error compensation structure cannot fully utilize available angular rate information, the invention provides an improved attitude algorithm coning error compensation structure so as to provide a novel angular rate input attitude algorithm structure. On the basis of defining the classical conical motion form and analyzing several necessary conical motion characteristics, the provided attitude algorithm coning error compensation structure is simplified to obtain a condensed attitude algorithm coning error compensation structure; a coning error compensation error criterion is defined, and the specific description of the error criterion is derived; a coning error compensation optimization object and a coning error compensation optimization method are selected, and parameter optimization designing on the coning e</description><subject>GYROSCOPIC INSTRUMENTS</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>SURVEYING</subject><subject>TESTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyj0KwkAQhuE0FqLeYTyAkLBoH4JiJQj2YciOycL-Mftt4-lN4QGsXnh4t82zj3P1rKQMIRdzBTHgUK0Q-zmpwxKoQOuEqqtFS5mVg0CUUoYL7sNwKdJKS7L7ZvNmX-Tw66453q6v4X6SnEYpmSeJgnF4dK25mLYz597883wBT_s4og</recordid><startdate>20140312</startdate><enddate>20140312</enddate><creator>TANG CHUANYE</creator><creator>LV CAIPING</creator><creator>FANG LIN</creator><creator>SONG RUI</creator><creator>CHEN XIYUAN</creator><creator>HUANG HAOQIAN</creator><creator>HE KUNPENG</creator><scope>EVB</scope></search><sort><creationdate>20140312</creationdate><title>Angular rate input attitude algorithm structure and parameter optimization method</title><author>TANG CHUANYE ; LV CAIPING ; FANG LIN ; SONG RUI ; CHEN XIYUAN ; HUANG HAOQIAN ; HE KUNPENG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN103630135A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2014</creationdate><topic>GYROSCOPIC INSTRUMENTS</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SURVEYING</topic><topic>TESTING</topic><toplevel>online_resources</toplevel><creatorcontrib>TANG CHUANYE</creatorcontrib><creatorcontrib>LV CAIPING</creatorcontrib><creatorcontrib>FANG LIN</creatorcontrib><creatorcontrib>SONG RUI</creatorcontrib><creatorcontrib>CHEN XIYUAN</creatorcontrib><creatorcontrib>HUANG HAOQIAN</creatorcontrib><creatorcontrib>HE KUNPENG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TANG CHUANYE</au><au>LV CAIPING</au><au>FANG LIN</au><au>SONG RUI</au><au>CHEN XIYUAN</au><au>HUANG HAOQIAN</au><au>HE KUNPENG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Angular rate input attitude algorithm structure and parameter optimization method</title><date>2014-03-12</date><risdate>2014</risdate><abstract>The invention discloses a novel angular rate input attitude algorithm structure and a parameter optimization method. Aiming at the problem that the traditional angular rate input attitude algorithm coning error compensation structure cannot fully utilize available angular rate information, the invention provides an improved attitude algorithm coning error compensation structure so as to provide a novel angular rate input attitude algorithm structure. On the basis of defining the classical conical motion form and analyzing several necessary conical motion characteristics, the provided attitude algorithm coning error compensation structure is simplified to obtain a condensed attitude algorithm coning error compensation structure; a coning error compensation error criterion is defined, and the specific description of the error criterion is derived; a coning error compensation optimization object and a coning error compensation optimization method are selected, and parameter optimization designing on the coning e</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN103630135A
source esp@cenet
subjects GYROSCOPIC INSTRUMENTS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
SURVEYING
TESTING
title Angular rate input attitude algorithm structure and parameter optimization method
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-08T00%3A07%3A12IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=TANG%20CHUANYE&rft.date=2014-03-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN103630135A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true