Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.
<p>Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.</p>
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلفون آخرون: | , , , |
| منشور في: |
2025
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| الموضوعات: | |
| الوسوم: |
إضافة وسم
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| _version_ | 1852015258051280896 |
|---|---|
| author | Muhammad Wasim (8319120) |
| author2 | Ahsan Ali (6478244) Faisal Saleem (1872289) Inam Ul Hasan Shaikh (11654934) Jamshed Iqbal (82302) |
| author2_role | author author author author |
| author_facet | Muhammad Wasim (8319120) Ahsan Ali (6478244) Faisal Saleem (1872289) Inam Ul Hasan Shaikh (11654934) Jamshed Iqbal (82302) |
| author_role | author |
| dc.creator.none.fl_str_mv | Muhammad Wasim (8319120) Ahsan Ali (6478244) Faisal Saleem (1872289) Inam Ul Hasan Shaikh (11654934) Jamshed Iqbal (82302) |
| dc.date.none.fl_str_mv | 2025-10-31T17:41:28Z |
| dc.identifier.none.fl_str_mv | 10.1371/journal.pone.0335392.g014 |
| dc.relation.none.fl_str_mv | https://figshare.com/articles/figure/Rate_of_change_of_accelerations_due_to_the_aerodynamic_forces_at_5_5_ms_sup_sup_sup_1_sup_speed_of_the_airship_/30503365 |
| dc.rights.none.fl_str_mv | CC BY 4.0 info:eu-repo/semantics/openAccess |
| dc.subject.none.fl_str_mv | Inorganic Chemistry Computational Biology Space Science Environmental Sciences not elsewhere classified Biological Sciences not elsewhere classified Mathematical Sciences not elsewhere classified Chemical Sciences not elsewhere classified Information Systems not elsewhere classified unscented kalman filter uncertain nonlinear dynamics sliding mode controller simulation results show hovering payload deliveries fully autonomous perspective estimated lumped uncertainty robust adaptive control lumped model uncertainty many potential applications trajectory tracking control lumped model uncertainties wind disturbance estimation lyapunov stability analysis airship trajectory tracking model uncertainties wind disturbance ultimate control desired trajectory applications require xlink "> usmc ), robotic airship research studies proposed method paper addresses method solves major challenge investigated using important aspects comprehensive algorithm chattering problem bound constraint airship autonomy aerostatic platform |
| dc.title.none.fl_str_mv | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| dc.type.none.fl_str_mv | Image Figure info:eu-repo/semantics/publishedVersion image |
| description | <p>Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.</p> |
| eu_rights_str_mv | openAccess |
| id | Manara_841d651da187d9bed2f38c7efa1d400a |
| identifier_str_mv | 10.1371/journal.pone.0335392.g014 |
| network_acronym_str | Manara |
| network_name_str | ManaraRepo |
| oai_identifier_str | oai:figshare.com:article/30503365 |
| publishDate | 2025 |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| rights_invalid_str_mv | CC BY 4.0 |
| spelling | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.Muhammad Wasim (8319120)Ahsan Ali (6478244)Faisal Saleem (1872289)Inam Ul Hasan Shaikh (11654934)Jamshed Iqbal (82302)Inorganic ChemistryComputational BiologySpace ScienceEnvironmental Sciences not elsewhere classifiedBiological Sciences not elsewhere classifiedMathematical Sciences not elsewhere classifiedChemical Sciences not elsewhere classifiedInformation Systems not elsewhere classifiedunscented kalman filteruncertain nonlinear dynamicssliding mode controllersimulation results showhovering payload deliveriesfully autonomous perspectiveestimated lumped uncertaintyrobust adaptive controllumped model uncertaintymany potential applicationstrajectory tracking controllumped model uncertaintieswind disturbance estimationlyapunov stability analysisairship trajectory trackingmodel uncertaintieswind disturbanceultimate controldesired trajectoryapplications requirexlink ">usmc ),robotic airshipresearch studiesproposed methodpaper addressesmethod solvesmajor challengeinvestigated usingimportant aspectscomprehensive algorithmchattering problembound constraintairship autonomyaerostatic platform<p>Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship.</p>2025-10-31T17:41:28ZImageFigureinfo:eu-repo/semantics/publishedVersionimage10.1371/journal.pone.0335392.g014https://figshare.com/articles/figure/Rate_of_change_of_accelerations_due_to_the_aerodynamic_forces_at_5_5_ms_sup_sup_sup_1_sup_speed_of_the_airship_/30503365CC BY 4.0info:eu-repo/semantics/openAccessoai:figshare.com:article/305033652025-10-31T17:41:28Z |
| spellingShingle | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. Muhammad Wasim (8319120) Inorganic Chemistry Computational Biology Space Science Environmental Sciences not elsewhere classified Biological Sciences not elsewhere classified Mathematical Sciences not elsewhere classified Chemical Sciences not elsewhere classified Information Systems not elsewhere classified unscented kalman filter uncertain nonlinear dynamics sliding mode controller simulation results show hovering payload deliveries fully autonomous perspective estimated lumped uncertainty robust adaptive control lumped model uncertainty many potential applications trajectory tracking control lumped model uncertainties wind disturbance estimation lyapunov stability analysis airship trajectory tracking model uncertainties wind disturbance ultimate control desired trajectory applications require xlink "> usmc ), robotic airship research studies proposed method paper addresses method solves major challenge investigated using important aspects comprehensive algorithm chattering problem bound constraint airship autonomy aerostatic platform |
| status_str | publishedVersion |
| title | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| title_full | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| title_fullStr | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| title_full_unstemmed | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| title_short | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| title_sort | Rate of change of accelerations due to the aerodynamic forces at 5.5 ms<sup>−</sup><sup>1</sup> speed of the airship. |
| topic | Inorganic Chemistry Computational Biology Space Science Environmental Sciences not elsewhere classified Biological Sciences not elsewhere classified Mathematical Sciences not elsewhere classified Chemical Sciences not elsewhere classified Information Systems not elsewhere classified unscented kalman filter uncertain nonlinear dynamics sliding mode controller simulation results show hovering payload deliveries fully autonomous perspective estimated lumped uncertainty robust adaptive control lumped model uncertainty many potential applications trajectory tracking control lumped model uncertainties wind disturbance estimation lyapunov stability analysis airship trajectory tracking model uncertainties wind disturbance ultimate control desired trajectory applications require xlink "> usmc ), robotic airship research studies proposed method paper addresses method solves major challenge investigated using important aspects comprehensive algorithm chattering problem bound constraint airship autonomy aerostatic platform |