Method of generating control command for aerial vehicle and system thereof
The present invention relates to a method and a system for generating a control command for an aircraft. One embodiment of the present invention provides the method for generating a control command for an aircraft equipped with a plurality of control wings and an optical fiber for wired data link. T...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; kor |
| 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 | UM TAE YOON PARK BONG GYUN |
| description | The present invention relates to a method and a system for generating a control command for an aircraft. One embodiment of the present invention provides the method for generating a control command for an aircraft equipped with a plurality of control wings and an optical fiber for wired data link. The method for generating a control command for an aircraft comprises: a step of determining a current speed of an aircraft; a step of determining maneuver displacements applied to each of a plurality of control vanes; a step of determining a first non-moving displacement based on a speed, a limit speed and a proportional gain (K); a step of determining a second non-moving displacement based on the first non-moving displacement and margin displacement; a step of generating a steering command based on the second non-moving displacement and the maneuver displacements; and a step of updating the speed of the aircraft and determining the first non-moving displacement or a step of repeating the step of generating the steering command. An objective of the present invention is to provide the method for generating a control command for an aircraft that generates a non-moving control command in a closed-loop control method.
본 발명은 비행체의 조종 명령 생성 방법 및 그 시스템에 관한 것으로, 본 발명의 일 실시예는 복수의 조종 날개들 및 유선 데이터 링크용 광섬유를 구비한 비행체의 조종 명령 생성 방법을 제공한다. 상기 비행체의 조종 명령 생성 방법은, 상기 비행체의 현재 속력(JPEG112020137442322-pat00321.jpg55)을 결정하는 단계, 상기 복수의 조종 날개들 각각에 적용되는 기동 변위들(JPEG112020137442322-pat00322.jpg521)을 결정하는 단계, 상기 속력(JPEG112020137442322-pat00323.jpg55), 제한 속력(JPEG112020137442322-pat00324.jpg53) 및 비례 이득(K)을 기초로, 제1 무기동 변위(JPEG112020137442322-pat00325.jpg55)를 결정하는 단계, 상기 제1 무기동 변위(JPEG112020137442322-pat00326.jpg55)와 여유 변위(JPEG112020137442322-pat00327.jpg522)를 기초로, 제2 무기동 변위(JPEG112020137442322-pat00328.jpg55)를 결정하는 단계, 상기 제2 무기동 변위(JPEG112020137442322-pat00329.jpg55)와 상기 기동 변위들(JPEG112020137442322-pat00330.jpg522)을 기초로, 조종 명령을 생성하는 단계, 및 상기 비행체의 상기 속력을 갱신하고, 상기 제1 무기동 변위(JPEG112020137442322-pat00331.jpg55)를 결정하는 단계 내지 상기 조종 명령 생성 단계를 반복하는 단계를 포함한다. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_KR102395893BB1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>KR102395893BB1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_KR102395893BB13</originalsourceid><addsrcrecordid>eNrjZPDyTS3JyE9RyE9TSE_NSy1KLMnMS1dIzs8rKcrPAdK5uYl5KQpp-UUKialFmYk5CmWpGZnJOakKIOHiyuKS1FyFkozUotT8NB4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJgMtKAk3jvI0MDI2NLUwtLYycnQmDhVAO_zNhk</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Method of generating control command for aerial vehicle and system thereof</title><source>esp@cenet</source><creator>UM TAE YOON ; PARK BONG GYUN</creator><creatorcontrib>UM TAE YOON ; PARK BONG GYUN</creatorcontrib><description>The present invention relates to a method and a system for generating a control command for an aircraft. One embodiment of the present invention provides the method for generating a control command for an aircraft equipped with a plurality of control wings and an optical fiber for wired data link. The method for generating a control command for an aircraft comprises: a step of determining a current speed of an aircraft; a step of determining maneuver displacements applied to each of a plurality of control vanes; a step of determining a first non-moving displacement based on a speed, a limit speed and a proportional gain (K); a step of determining a second non-moving displacement based on the first non-moving displacement and margin displacement; a step of generating a steering command based on the second non-moving displacement and the maneuver displacements; and a step of updating the speed of the aircraft and determining the first non-moving displacement or a step of repeating the step of generating the steering command. An objective of the present invention is to provide the method for generating a control command for an aircraft that generates a non-moving control command in a closed-loop control method.
본 발명은 비행체의 조종 명령 생성 방법 및 그 시스템에 관한 것으로, 본 발명의 일 실시예는 복수의 조종 날개들 및 유선 데이터 링크용 광섬유를 구비한 비행체의 조종 명령 생성 방법을 제공한다. 상기 비행체의 조종 명령 생성 방법은, 상기 비행체의 현재 속력(JPEG112020137442322-pat00321.jpg55)을 결정하는 단계, 상기 복수의 조종 날개들 각각에 적용되는 기동 변위들(JPEG112020137442322-pat00322.jpg521)을 결정하는 단계, 상기 속력(JPEG112020137442322-pat00323.jpg55), 제한 속력(JPEG112020137442322-pat00324.jpg53) 및 비례 이득(K)을 기초로, 제1 무기동 변위(JPEG112020137442322-pat00325.jpg55)를 결정하는 단계, 상기 제1 무기동 변위(JPEG112020137442322-pat00326.jpg55)와 여유 변위(JPEG112020137442322-pat00327.jpg522)를 기초로, 제2 무기동 변위(JPEG112020137442322-pat00328.jpg55)를 결정하는 단계, 상기 제2 무기동 변위(JPEG112020137442322-pat00329.jpg55)와 상기 기동 변위들(JPEG112020137442322-pat00330.jpg522)을 기초로, 조종 명령을 생성하는 단계, 및 상기 비행체의 상기 속력을 갱신하고, 상기 제1 무기동 변위(JPEG112020137442322-pat00331.jpg55)를 결정하는 단계 내지 상기 조종 명령 생성 단계를 반복하는 단계를 포함한다.</description><language>eng ; kor</language><subject>AIMING ; AMMUNITION ; BLASTING ; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPON SIGHTS ; WEAPONS</subject><creationdate>2022</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=20220509&DB=EPODOC&CC=KR&NR=102395893B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220509&DB=EPODOC&CC=KR&NR=102395893B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>UM TAE YOON</creatorcontrib><creatorcontrib>PARK BONG GYUN</creatorcontrib><title>Method of generating control command for aerial vehicle and system thereof</title><description>The present invention relates to a method and a system for generating a control command for an aircraft. One embodiment of the present invention provides the method for generating a control command for an aircraft equipped with a plurality of control wings and an optical fiber for wired data link. The method for generating a control command for an aircraft comprises: a step of determining a current speed of an aircraft; a step of determining maneuver displacements applied to each of a plurality of control vanes; a step of determining a first non-moving displacement based on a speed, a limit speed and a proportional gain (K); a step of determining a second non-moving displacement based on the first non-moving displacement and margin displacement; a step of generating a steering command based on the second non-moving displacement and the maneuver displacements; and a step of updating the speed of the aircraft and determining the first non-moving displacement or a step of repeating the step of generating the steering command. An objective of the present invention is to provide the method for generating a control command for an aircraft that generates a non-moving control command in a closed-loop control method.
본 발명은 비행체의 조종 명령 생성 방법 및 그 시스템에 관한 것으로, 본 발명의 일 실시예는 복수의 조종 날개들 및 유선 데이터 링크용 광섬유를 구비한 비행체의 조종 명령 생성 방법을 제공한다. 상기 비행체의 조종 명령 생성 방법은, 상기 비행체의 현재 속력(JPEG112020137442322-pat00321.jpg55)을 결정하는 단계, 상기 복수의 조종 날개들 각각에 적용되는 기동 변위들(JPEG112020137442322-pat00322.jpg521)을 결정하는 단계, 상기 속력(JPEG112020137442322-pat00323.jpg55), 제한 속력(JPEG112020137442322-pat00324.jpg53) 및 비례 이득(K)을 기초로, 제1 무기동 변위(JPEG112020137442322-pat00325.jpg55)를 결정하는 단계, 상기 제1 무기동 변위(JPEG112020137442322-pat00326.jpg55)와 여유 변위(JPEG112020137442322-pat00327.jpg522)를 기초로, 제2 무기동 변위(JPEG112020137442322-pat00328.jpg55)를 결정하는 단계, 상기 제2 무기동 변위(JPEG112020137442322-pat00329.jpg55)와 상기 기동 변위들(JPEG112020137442322-pat00330.jpg522)을 기초로, 조종 명령을 생성하는 단계, 및 상기 비행체의 상기 속력을 갱신하고, 상기 제1 무기동 변위(JPEG112020137442322-pat00331.jpg55)를 결정하는 단계 내지 상기 조종 명령 생성 단계를 반복하는 단계를 포함한다.</description><subject>AIMING</subject><subject>AMMUNITION</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPON SIGHTS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPDyTS3JyE9RyE9TSE_NSy1KLMnMS1dIzs8rKcrPAdK5uYl5KQpp-UUKialFmYk5CmWpGZnJOakKIOHiyuKS1FyFkozUotT8NB4G1rTEnOJUXijNzaDs5hri7KGbWpAfn1pckJgMtKAk3jvI0MDI2NLUwtLYycnQmDhVAO_zNhk</recordid><startdate>20220509</startdate><enddate>20220509</enddate><creator>UM TAE YOON</creator><creator>PARK BONG GYUN</creator><scope>EVB</scope></search><sort><creationdate>20220509</creationdate><title>Method of generating control command for aerial vehicle and system thereof</title><author>UM TAE YOON ; PARK BONG GYUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR102395893BB13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2022</creationdate><topic>AIMING</topic><topic>AMMUNITION</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPON SIGHTS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>UM TAE YOON</creatorcontrib><creatorcontrib>PARK BONG GYUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>UM TAE YOON</au><au>PARK BONG GYUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method of generating control command for aerial vehicle and system thereof</title><date>2022-05-09</date><risdate>2022</risdate><abstract>The present invention relates to a method and a system for generating a control command for an aircraft. One embodiment of the present invention provides the method for generating a control command for an aircraft equipped with a plurality of control wings and an optical fiber for wired data link. The method for generating a control command for an aircraft comprises: a step of determining a current speed of an aircraft; a step of determining maneuver displacements applied to each of a plurality of control vanes; a step of determining a first non-moving displacement based on a speed, a limit speed and a proportional gain (K); a step of determining a second non-moving displacement based on the first non-moving displacement and margin displacement; a step of generating a steering command based on the second non-moving displacement and the maneuver displacements; and a step of updating the speed of the aircraft and determining the first non-moving displacement or a step of repeating the step of generating the steering command. An objective of the present invention is to provide the method for generating a control command for an aircraft that generates a non-moving control command in a closed-loop control method.
본 발명은 비행체의 조종 명령 생성 방법 및 그 시스템에 관한 것으로, 본 발명의 일 실시예는 복수의 조종 날개들 및 유선 데이터 링크용 광섬유를 구비한 비행체의 조종 명령 생성 방법을 제공한다. 상기 비행체의 조종 명령 생성 방법은, 상기 비행체의 현재 속력(JPEG112020137442322-pat00321.jpg55)을 결정하는 단계, 상기 복수의 조종 날개들 각각에 적용되는 기동 변위들(JPEG112020137442322-pat00322.jpg521)을 결정하는 단계, 상기 속력(JPEG112020137442322-pat00323.jpg55), 제한 속력(JPEG112020137442322-pat00324.jpg53) 및 비례 이득(K)을 기초로, 제1 무기동 변위(JPEG112020137442322-pat00325.jpg55)를 결정하는 단계, 상기 제1 무기동 변위(JPEG112020137442322-pat00326.jpg55)와 여유 변위(JPEG112020137442322-pat00327.jpg522)를 기초로, 제2 무기동 변위(JPEG112020137442322-pat00328.jpg55)를 결정하는 단계, 상기 제2 무기동 변위(JPEG112020137442322-pat00329.jpg55)와 상기 기동 변위들(JPEG112020137442322-pat00330.jpg522)을 기초로, 조종 명령을 생성하는 단계, 및 상기 비행체의 상기 속력을 갱신하고, 상기 제1 무기동 변위(JPEG112020137442322-pat00331.jpg55)를 결정하는 단계 내지 상기 조종 명령 생성 단계를 반복하는 단계를 포함한다.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; kor |
| recordid | cdi_epo_espacenet_KR102395893BB1 |
| source | esp@cenet |
| subjects | AIMING AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPON SIGHTS WEAPONS |
| title | Method of generating control command for aerial vehicle and system thereof |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T07%3A09%3A03IST&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=UM%20TAE%20YOON&rft.date=2022-05-09&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EKR102395893BB1%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 |