Aircraft control surface deflection angle measuring method
The invention discloses an aircraft control surface deflection angle measuring method. The method comprises the following steps of pasting mark points on an aircraft control surface and other parts, measuring the motion space track of the mark points pasted on the aircraft control surface by using a...
Gespeichert in:
| Hauptverfasser: | , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| 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 | HOU BAIYU ZHAO PEI ZHENG BO XIE YUN LIU YANGZHI ZHANG YONGJIAN NI CHENG DING GUOPING |
| description | The invention discloses an aircraft control surface deflection angle measuring method. The method comprises the following steps of pasting mark points on an aircraft control surface and other parts, measuring the motion space track of the mark points pasted on the aircraft control surface by using an industrial photogrammetric camera, and taking the mark points of other parts of an aircraft as reference points; and obtaining space coordinates of the mark points on the control surface in each state, simulating the motion tracks of the mark points, determining the rotation axis of the aircraft control surface, drawing a vertical line from the mark points to the rotation axis of the control surface in each deflection state, and taking the included angle of the vertical line of a single mark point in different states as the deflection angle of the aircraft control surface. According to the invention, the variable quantity of the deflection angle of the control surface can be displayed in real time, the problems o |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN112729221A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN112729221A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN112729221A3</originalsourceid><addsrcrecordid>eNrjZLByzCxKLkpMK1FIzs8rKcrPUSguLUpLTE5VSElNy0lNLsnMz1NIzEvPSVXITU0EymXmpQNZJRn5KTwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4AGhIXmpJvLOfoaGRuZGlkZGhozExagCgfi9d</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft control surface deflection angle measuring method</title><source>esp@cenet</source><creator>HOU BAIYU ; ZHAO PEI ; ZHENG BO ; XIE YUN ; LIU YANGZHI ; ZHANG YONGJIAN ; NI CHENG ; DING GUOPING</creator><creatorcontrib>HOU BAIYU ; ZHAO PEI ; ZHENG BO ; XIE YUN ; LIU YANGZHI ; ZHANG YONGJIAN ; NI CHENG ; DING GUOPING</creatorcontrib><description>The invention discloses an aircraft control surface deflection angle measuring method. The method comprises the following steps of pasting mark points on an aircraft control surface and other parts, measuring the motion space track of the mark points pasted on the aircraft control surface by using an industrial photogrammetric camera, and taking the mark points of other parts of an aircraft as reference points; and obtaining space coordinates of the mark points on the control surface in each state, simulating the motion tracks of the mark points, determining the rotation axis of the aircraft control surface, drawing a vertical line from the mark points to the rotation axis of the control surface in each deflection state, and taking the included angle of the vertical line of a single mark point in different states as the deflection angle of the aircraft control surface. According to the invention, the variable quantity of the deflection angle of the control surface can be displayed in real time, the problems o</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; GYROSCOPIC INSTRUMENTS ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PERFORMING OPERATIONS ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SURVEYING ; TESTING ; TRANSPORTING</subject><creationdate>2021</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&date=20210430&DB=EPODOC&CC=CN&NR=112729221A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210430&DB=EPODOC&CC=CN&NR=112729221A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOU BAIYU</creatorcontrib><creatorcontrib>ZHAO PEI</creatorcontrib><creatorcontrib>ZHENG BO</creatorcontrib><creatorcontrib>XIE YUN</creatorcontrib><creatorcontrib>LIU YANGZHI</creatorcontrib><creatorcontrib>ZHANG YONGJIAN</creatorcontrib><creatorcontrib>NI CHENG</creatorcontrib><creatorcontrib>DING GUOPING</creatorcontrib><title>Aircraft control surface deflection angle measuring method</title><description>The invention discloses an aircraft control surface deflection angle measuring method. The method comprises the following steps of pasting mark points on an aircraft control surface and other parts, measuring the motion space track of the mark points pasted on the aircraft control surface by using an industrial photogrammetric camera, and taking the mark points of other parts of an aircraft as reference points; and obtaining space coordinates of the mark points on the control surface in each state, simulating the motion tracks of the mark points, determining the rotation axis of the aircraft control surface, drawing a vertical line from the mark points to the rotation axis of the control surface in each deflection state, and taking the included angle of the vertical line of a single mark point in different states as the deflection angle of the aircraft control surface. According to the invention, the variable quantity of the deflection angle of the control surface can be displayed in real time, the problems o</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>GYROSCOPIC INSTRUMENTS</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PERFORMING OPERATIONS</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>SURVEYING</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByzCxKLkpMK1FIzs8rKcrPUSguLUpLTE5VSElNy0lNLsnMz1NIzEvPSVXITU0EymXmpQNZJRn5KTwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4AGhIXmpJvLOfoaGRuZGlkZGhozExagCgfi9d</recordid><startdate>20210430</startdate><enddate>20210430</enddate><creator>HOU BAIYU</creator><creator>ZHAO PEI</creator><creator>ZHENG BO</creator><creator>XIE YUN</creator><creator>LIU YANGZHI</creator><creator>ZHANG YONGJIAN</creator><creator>NI CHENG</creator><creator>DING GUOPING</creator><scope>EVB</scope></search><sort><creationdate>20210430</creationdate><title>Aircraft control surface deflection angle measuring method</title><author>HOU BAIYU ; ZHAO PEI ; ZHENG BO ; XIE YUN ; LIU YANGZHI ; ZHANG YONGJIAN ; NI CHENG ; DING GUOPING</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112729221A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>GYROSCOPIC INSTRUMENTS</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PERFORMING OPERATIONS</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SURVEYING</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>HOU BAIYU</creatorcontrib><creatorcontrib>ZHAO PEI</creatorcontrib><creatorcontrib>ZHENG BO</creatorcontrib><creatorcontrib>XIE YUN</creatorcontrib><creatorcontrib>LIU YANGZHI</creatorcontrib><creatorcontrib>ZHANG YONGJIAN</creatorcontrib><creatorcontrib>NI CHENG</creatorcontrib><creatorcontrib>DING GUOPING</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOU BAIYU</au><au>ZHAO PEI</au><au>ZHENG BO</au><au>XIE YUN</au><au>LIU YANGZHI</au><au>ZHANG YONGJIAN</au><au>NI CHENG</au><au>DING GUOPING</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft control surface deflection angle measuring method</title><date>2021-04-30</date><risdate>2021</risdate><abstract>The invention discloses an aircraft control surface deflection angle measuring method. The method comprises the following steps of pasting mark points on an aircraft control surface and other parts, measuring the motion space track of the mark points pasted on the aircraft control surface by using an industrial photogrammetric camera, and taking the mark points of other parts of an aircraft as reference points; and obtaining space coordinates of the mark points on the control surface in each state, simulating the motion tracks of the mark points, determining the rotation axis of the aircraft control surface, drawing a vertical line from the mark points to the rotation axis of the control surface in each deflection state, and taking the included angle of the vertical line of a single mark point in different states as the deflection angle of the aircraft control surface. According to the invention, the variable quantity of the deflection angle of the control surface can be displayed in real time, the problems o</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN112729221A |
| source | esp@cenet |
| subjects | AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT GYROSCOPIC INSTRUMENTS HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING TRANSPORTING |
| title | Aircraft control surface deflection angle measuring method |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T21%3A51%3A14IST&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=HOU%20BAIYU&rft.date=2021-04-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112729221A%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 |