Agent-Based Dynamically Reconfigurable Missile Modelling
In this study, an air platform dynamic model that hasthe ability to maneuver in all axes (displacement and rotation) and to followanother aircraft is modeled. Rigid aircraft mathematical models is adopted forthe model aircraft and the calculations are done in a generic way except foraeroelasticity e...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Sakarya University
2018-10-01
|
| Series: | Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi |
| Subjects: | |
| Online Access: | https://dergipark.org.tr/tr/download/article-file/509881 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1846111553115389952 |
|---|---|
| author | Mehmet Fatih Hocaoğlu İlyas Kandemir |
| author_facet | Mehmet Fatih Hocaoğlu İlyas Kandemir |
| author_sort | Mehmet Fatih Hocaoğlu |
| collection | DOAJ |
| description | In this study, an air platform dynamic model that hasthe ability to maneuver in all axes (displacement and rotation) and to followanother aircraft is modeled. Rigid aircraft mathematical models is adopted forthe model aircraft and the calculations are done in a generic way except foraeroelasticity effects. In consideration of the geodesic structure of theearth, the gravity model is also designed accordingly and the atmosphericconditions at a given altitude are included in the calculations. The createdair platforms are dynamically changed in degrees of freedom in accordance withthe analysis purposes, under the defined scenario conditions. For missilemodels, the definition of the configuration including phase definitions, engineselections and customization of engine properties, seeker activation scheduleand fuse type are user-defined supported by an interface. Phase transitioncontrols, motor controls, sensor opening and closing decisions are rule-basedand reasoning-based. To be able to enhance modeling flexibility and inject areasoning capability, the models are designed as intelligent agents and theyare modeled in Agent driven simulation framework (AdSiF). |
| format | Article |
| id | doaj-art-7d6ede74fa6643c085d4ab89b5b589d3 |
| institution | Kabale University |
| issn | 2147-835X |
| language | English |
| publishDate | 2018-10-01 |
| publisher | Sakarya University |
| record_format | Article |
| series | Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi |
| spelling | doaj-art-7d6ede74fa6643c085d4ab89b5b589d32024-12-23T07:58:48ZengSakarya UniversitySakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi2147-835X2018-10-012251466147610.16984/saufenbilder.40264728Agent-Based Dynamically Reconfigurable Missile ModellingMehmet Fatih Hocaoğluhttps://orcid.org/0000-0001-7428-9351İlyas Kandemirhttps://orcid.org/0000-0002-8773-6541In this study, an air platform dynamic model that hasthe ability to maneuver in all axes (displacement and rotation) and to followanother aircraft is modeled. Rigid aircraft mathematical models is adopted forthe model aircraft and the calculations are done in a generic way except foraeroelasticity effects. In consideration of the geodesic structure of theearth, the gravity model is also designed accordingly and the atmosphericconditions at a given altitude are included in the calculations. The createdair platforms are dynamically changed in degrees of freedom in accordance withthe analysis purposes, under the defined scenario conditions. For missilemodels, the definition of the configuration including phase definitions, engineselections and customization of engine properties, seeker activation scheduleand fuse type are user-defined supported by an interface. Phase transitioncontrols, motor controls, sensor opening and closing decisions are rule-basedand reasoning-based. To be able to enhance modeling flexibility and inject areasoning capability, the models are designed as intelligent agents and theyare modeled in Agent driven simulation framework (AdSiF).https://dergipark.org.tr/tr/download/article-file/509881adsifagent based simulationair defenseaircraft modelingmissile modelingsix axis motion |
| spellingShingle | Mehmet Fatih Hocaoğlu İlyas Kandemir Agent-Based Dynamically Reconfigurable Missile Modelling Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi adsif agent based simulation air defense aircraft modeling missile modeling six axis motion |
| title | Agent-Based Dynamically Reconfigurable Missile Modelling |
| title_full | Agent-Based Dynamically Reconfigurable Missile Modelling |
| title_fullStr | Agent-Based Dynamically Reconfigurable Missile Modelling |
| title_full_unstemmed | Agent-Based Dynamically Reconfigurable Missile Modelling |
| title_short | Agent-Based Dynamically Reconfigurable Missile Modelling |
| title_sort | agent based dynamically reconfigurable missile modelling |
| topic | adsif agent based simulation air defense aircraft modeling missile modeling six axis motion |
| url | https://dergipark.org.tr/tr/download/article-file/509881 |
| work_keys_str_mv | AT mehmetfatihhocaoglu agentbaseddynamicallyreconfigurablemissilemodelling AT ilyaskandemir agentbaseddynamicallyreconfigurablemissilemodelling |