Eintrag weiter verarbeiten
Aircraft Controller Flight Control System Design
Gespeichert in:
Zeitschriftentitel: | Applied Mechanics and Materials |
---|---|
Personen und Körperschaften: | , |
In: | Applied Mechanics and Materials, 602-605, 2014, S. 1291-1294 |
Format: | E-Article |
Sprache: | Unbestimmt |
veröffentlicht: |
Trans Tech Publications, Ltd.
|
Schlagwörter: |
author_facet |
Zhou, Hong Cheng Wang, Dao Bao Zhou, Hong Cheng Wang, Dao Bao |
---|---|
author |
Zhou, Hong Cheng Wang, Dao Bao |
spellingShingle |
Zhou, Hong Cheng Wang, Dao Bao Applied Mechanics and Materials Aircraft Controller Flight Control System Design General Engineering |
author_sort |
zhou, hong cheng |
spelling |
Zhou, Hong Cheng Wang, Dao Bao 1662-7482 Trans Tech Publications, Ltd. General Engineering http://dx.doi.org/10.4028/www.scientific.net/amm.602-605.1291 <jats:p>The servo control methods of motion configuration are researched. Based on analysis for characteristic of the motion configuration, the control strategy and control law used on the motion control system are presented. The controllers are respectively designed by frequency correcting method and normal control method which belongs to classical control theory. Sliding mode variable structure control method is presented for location control law designing, so that the problem of location control loop low velocity creeping is solved, and a simulating experimentation demonstrate the effectiveness of the proposed approach.</jats:p> Aircraft Controller Flight Control System Design Applied Mechanics and Materials |
doi_str_mv |
10.4028/www.scientific.net/amm.602-605.1291 |
facet_avail |
Online |
format |
ElectronicArticle |
fullrecord |
blob:ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuNDAyOC93d3cuc2NpZW50aWZpYy5uZXQvYW1tLjYwMi02MDUuMTI5MQ |
id |
ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuNDAyOC93d3cuc2NpZW50aWZpYy5uZXQvYW1tLjYwMi02MDUuMTI5MQ |
institution |
DE-Gla1 DE-Zi4 DE-15 DE-Pl11 DE-Rs1 DE-105 DE-14 DE-Ch1 DE-L229 DE-D275 DE-Bn3 DE-Brt1 DE-D161 |
imprint |
Trans Tech Publications, Ltd., 2014 |
imprint_str_mv |
Trans Tech Publications, Ltd., 2014 |
issn |
1662-7482 |
issn_str_mv |
1662-7482 |
language |
Undetermined |
mega_collection |
Trans Tech Publications, Ltd. (CrossRef) |
match_str |
zhou2014aircraftcontrollerflightcontrolsystemdesign |
publishDateSort |
2014 |
publisher |
Trans Tech Publications, Ltd. |
recordtype |
ai |
record_format |
ai |
series |
Applied Mechanics and Materials |
source_id |
49 |
title |
Aircraft Controller Flight Control System Design |
title_unstemmed |
Aircraft Controller Flight Control System Design |
title_full |
Aircraft Controller Flight Control System Design |
title_fullStr |
Aircraft Controller Flight Control System Design |
title_full_unstemmed |
Aircraft Controller Flight Control System Design |
title_short |
Aircraft Controller Flight Control System Design |
title_sort |
aircraft controller flight control system design |
topic |
General Engineering |
url |
http://dx.doi.org/10.4028/www.scientific.net/amm.602-605.1291 |
publishDate |
2014 |
physical |
1291-1294 |
description |
<jats:p>The servo control methods of motion configuration are researched. Based on analysis for characteristic of the motion configuration, the control strategy and control law used on the motion control system are presented. The controllers are respectively designed by frequency correcting method and normal control method which belongs to classical control theory. Sliding mode variable structure control method is presented for location control law designing, so that the problem of location control loop low velocity creeping is solved, and a simulating experimentation demonstrate the effectiveness of the proposed approach.</jats:p> |
container_start_page |
1291 |
container_title |
Applied Mechanics and Materials |
container_volume |
602-605 |
format_de105 |
Article, E-Article |
format_de14 |
Article, E-Article |
format_de15 |
Article, E-Article |
format_de520 |
Article, E-Article |
format_de540 |
Article, E-Article |
format_dech1 |
Article, E-Article |
format_ded117 |
Article, E-Article |
format_degla1 |
E-Article |
format_del152 |
Buch |
format_del189 |
Article, E-Article |
format_dezi4 |
Article |
format_dezwi2 |
Article, E-Article |
format_finc |
Article, E-Article |
format_nrw |
Article, E-Article |
_version_ |
1792327131336802304 |
geogr_code |
not assigned |
last_indexed |
2024-03-01T12:32:31.548Z |
geogr_code_person |
not assigned |
openURL |
url_ver=Z39.88-2004&ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fvufind.svn.sourceforge.net%3Agenerator&rft.title=Aircraft+Controller+Flight+Control+System+Design&rft.date=2014-08-01&genre=article&issn=1662-7482&volume=602-605&spage=1291&epage=1294&pages=1291-1294&jtitle=Applied+Mechanics+and+Materials&atitle=Aircraft+Controller+Flight+Control+System+Design&aulast=Wang&aufirst=Dao+Bao&rft_id=info%3Adoi%2F10.4028%2Fwww.scientific.net%2Famm.602-605.1291&rft.language%5B0%5D=und |
SOLR | |
_version_ | 1792327131336802304 |
author | Zhou, Hong Cheng, Wang, Dao Bao |
author_facet | Zhou, Hong Cheng, Wang, Dao Bao, Zhou, Hong Cheng, Wang, Dao Bao |
author_sort | zhou, hong cheng |
container_start_page | 1291 |
container_title | Applied Mechanics and Materials |
container_volume | 602-605 |
description | <jats:p>The servo control methods of motion configuration are researched. Based on analysis for characteristic of the motion configuration, the control strategy and control law used on the motion control system are presented. The controllers are respectively designed by frequency correcting method and normal control method which belongs to classical control theory. Sliding mode variable structure control method is presented for location control law designing, so that the problem of location control loop low velocity creeping is solved, and a simulating experimentation demonstrate the effectiveness of the proposed approach.</jats:p> |
doi_str_mv | 10.4028/www.scientific.net/amm.602-605.1291 |
facet_avail | Online |
format | ElectronicArticle |
format_de105 | Article, E-Article |
format_de14 | Article, E-Article |
format_de15 | Article, E-Article |
format_de520 | Article, E-Article |
format_de540 | Article, E-Article |
format_dech1 | Article, E-Article |
format_ded117 | Article, E-Article |
format_degla1 | E-Article |
format_del152 | Buch |
format_del189 | Article, E-Article |
format_dezi4 | Article |
format_dezwi2 | Article, E-Article |
format_finc | Article, E-Article |
format_nrw | Article, E-Article |
geogr_code | not assigned |
geogr_code_person | not assigned |
id | ai-49-aHR0cDovL2R4LmRvaS5vcmcvMTAuNDAyOC93d3cuc2NpZW50aWZpYy5uZXQvYW1tLjYwMi02MDUuMTI5MQ |
imprint | Trans Tech Publications, Ltd., 2014 |
imprint_str_mv | Trans Tech Publications, Ltd., 2014 |
institution | DE-Gla1, DE-Zi4, DE-15, DE-Pl11, DE-Rs1, DE-105, DE-14, DE-Ch1, DE-L229, DE-D275, DE-Bn3, DE-Brt1, DE-D161 |
issn | 1662-7482 |
issn_str_mv | 1662-7482 |
language | Undetermined |
last_indexed | 2024-03-01T12:32:31.548Z |
match_str | zhou2014aircraftcontrollerflightcontrolsystemdesign |
mega_collection | Trans Tech Publications, Ltd. (CrossRef) |
physical | 1291-1294 |
publishDate | 2014 |
publishDateSort | 2014 |
publisher | Trans Tech Publications, Ltd. |
record_format | ai |
recordtype | ai |
series | Applied Mechanics and Materials |
source_id | 49 |
spelling | Zhou, Hong Cheng Wang, Dao Bao 1662-7482 Trans Tech Publications, Ltd. General Engineering http://dx.doi.org/10.4028/www.scientific.net/amm.602-605.1291 <jats:p>The servo control methods of motion configuration are researched. Based on analysis for characteristic of the motion configuration, the control strategy and control law used on the motion control system are presented. The controllers are respectively designed by frequency correcting method and normal control method which belongs to classical control theory. Sliding mode variable structure control method is presented for location control law designing, so that the problem of location control loop low velocity creeping is solved, and a simulating experimentation demonstrate the effectiveness of the proposed approach.</jats:p> Aircraft Controller Flight Control System Design Applied Mechanics and Materials |
spellingShingle | Zhou, Hong Cheng, Wang, Dao Bao, Applied Mechanics and Materials, Aircraft Controller Flight Control System Design, General Engineering |
title | Aircraft Controller Flight Control System Design |
title_full | Aircraft Controller Flight Control System Design |
title_fullStr | Aircraft Controller Flight Control System Design |
title_full_unstemmed | Aircraft Controller Flight Control System Design |
title_short | Aircraft Controller Flight Control System Design |
title_sort | aircraft controller flight control system design |
title_unstemmed | Aircraft Controller Flight Control System Design |
topic | General Engineering |
url | http://dx.doi.org/10.4028/www.scientific.net/amm.602-605.1291 |