UAV AIRCRAFT MODEL FOR CONTROL SYSTEM FAILURES ANALYSIS
| Main Authors: | Żugaj, Marcin, Bibik, Przemysław, Jacewicz, Mariusz |
|---|---|
| Format: | Article |
| Terbitan: |
, 2017
|
| Subjects: | |
| Online Access: |
https://zenodo.org/record/1120055 |
| ctrlnum |
1120055 |
|---|---|
| fullrecord |
<?xml version="1.0"?>
<dc schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd"><creator>Żugaj, Marcin</creator><creator>Bibik, Przemysław</creator><creator>Jacewicz, Mariusz</creator><date>2017-12-20</date><description>In the paper, influence of control surface failures on UAV aircraft dynamics is investigated. A method for control loads determination for a nonlinear UAV aircraft model is presented. The model has been developed to analyse the influence of various control surface failures on aircraft controllability and to form the background for developing reconfiguration methods of flight control systems. The analysis of the control system failure impact on the aircraft dynamics and the ability of the control system to reconfiguration are presented.</description><identifier>https://zenodo.org/record/1120055</identifier><identifier>10.15632/jtam-pl.54.4.1405</identifier><identifier>oai:zenodo.org:1120055</identifier><rights>info:eu-repo/semantics/openAccess</rights><rights>https://creativecommons.org/licenses/by-nc/4.0/legalcode</rights><source>Journal of Theoretical and Applied Mechanics 54(4)</source><subject>UAV</subject><subject>flight dynamics</subject><subject>control</subject><subject>reconfiguration</subject><title>UAV AIRCRAFT MODEL FOR CONTROL SYSTEM FAILURES ANALYSIS</title><type>Journal:Article</type><type>Journal:Article</type><recordID>1120055</recordID></dc>
|
| format |
Journal:Article Journal |
| author |
Żugaj, Marcin Bibik, Przemysław Jacewicz, Mariusz |
| title |
UAV AIRCRAFT MODEL FOR CONTROL SYSTEM FAILURES ANALYSIS |
| publishDate |
2017 |
| topic |
UAV flight dynamics control reconfiguration |
| url |
https://zenodo.org/record/1120055 |
| contents |
In the paper, influence of control surface failures on UAV aircraft dynamics is investigated. A method for control loads determination for a nonlinear UAV aircraft model is presented. The model has been developed to analyse the influence of various control surface failures on aircraft controllability and to form the background for developing reconfiguration methods of flight control systems. The analysis of the control system failure impact on the aircraft dynamics and the ability of the control system to reconfiguration are presented. |
| id |
IOS16997.1120055 |
| institution |
DEFAULT |
| institution_type |
library:public library |
| library |
DEFAULT |
| collection |
DEFAULT |
| city |
DEFAULT |
| province |
DEFAULT |
| repoId |
IOS16997 |
| first_indexed |
2022-06-06T05:19:42Z |
| last_indexed |
2022-06-06T05:19:42Z |
| recordtype |
dc |
| merged_child_boolean |
1 |
| _version_ |
1739484025230196736 |
| score |
17.610285 |