In this study, an air platform dynamic model that has the ability to maneuver in all axes (displacement and rotation) and to follow another aircraft is modeled. Rigid aircraft mathematical models is adopted for the model aircraft and the calculations are done in a generic way except for aeroelasticity effects. In consideration of the geodesic structure of the earth, the gravity model is also designed accordingly and the atmospheric conditions at a given altitude are included in the calculations. The created air platforms are dynamically changed in degrees of freedom in accordance with the analysis purposes, under the defined scenario conditions. For missile models, the definition of the configuration including phase definitions, engine selections and customization of engine properties, seeker activation schedule and fuse type are user-defined supported by an interface. Phase transition controls, motor controls, sensor opening and closing decisions are rule-based and reasoning-based. To be able to enhance modeling flexibility and inject a reasoning capability, the models are designed as intelligent agents and they are modeled in Agent driven simulation framework (AdSiF).
Birincil Dil | en |
---|---|
Konular | Endüstri Mühendisliği, Mühendislik, Makine, Bilgisayar Bilimleri, Bilgi Sistemleri |
Yayımlanma Tarihi | October 2018 |
Dergi Bölümü | Araştırma Makalesi |
Yazarlar |
|
Bibtex | @araştırma makalesi { saufenbilder402647,
journal = {Sakarya University Journal of Science},
issn = {1301-4048},
eissn = {2147-835X},
address = {Sakarya Üniversitesi},
year = {2018},
volume = {22},
pages = {1466 - 1476},
doi = {10.16984/saufenbilder.402647},
title = {Agent-Based Dynamically Reconfigurable Missile Modelling},
key = {cite},
author = {Kandemir, İlyas and Hocaoğlu, Mehmet Fatih}
} |
APA | Hocaoğlu, M , Kandemir, İ . (2018). Agent-Based Dynamically Reconfigurable Missile Modelling. Sakarya University Journal of Science, 22 (5), 1466-1476. DOI: 10.16984/saufenbilder.402647 |
MLA | Hocaoğlu, M , Kandemir, İ . "Agent-Based Dynamically Reconfigurable Missile Modelling". Sakarya University Journal of Science 22 (2018): 1466-1476 <http://www.saujs.sakarya.edu.tr/issue/31265/402647> |
Chicago | Hocaoğlu, M , Kandemir, İ . "Agent-Based Dynamically Reconfigurable Missile Modelling". Sakarya University Journal of Science 22 (2018): 1466-1476 |
RIS | TY - JOUR T1 - Agent-Based Dynamically Reconfigurable Missile Modelling AU - Mehmet Fatih Hocaoğlu , İlyas Kandemir Y1 - 2018 PY - 2018 N1 - doi: 10.16984/saufenbilder.402647 DO - 10.16984/saufenbilder.402647 T2 - Sakarya University Journal of Science JF - Journal JO - JOR SP - 1466 EP - 1476 VL - 22 IS - 5 SN - 1301-4048-2147-835X M3 - doi: 10.16984/saufenbilder.402647 UR - http://dx.doi.org/10.16984/saufenbilder.402647 Y2 - 2018 ER - |
EndNote | %0 Sakarya University Journal of Science Agent-Based Dynamically Reconfigurable Missile Modelling %A Mehmet Fatih Hocaoğlu , İlyas Kandemir %T Agent-Based Dynamically Reconfigurable Missile Modelling %D 2018 %J Sakarya University Journal of Science %P 1301-4048-2147-835X %V 22 %N 5 %R doi: 10.16984/saufenbilder.402647 %U 10.16984/saufenbilder.402647 |
ISNAD | Hocaoğlu, Mehmet Fatih , Kandemir, İlyas . "Agent-Based Dynamically Reconfigurable Missile Modelling". Sakarya University Journal of Science 22 / 5 (Ekim 2018): 1466-1476. http://dx.doi.org/10.16984/saufenbilder.402647 |