Araştırma Makalesi
BibTex RIS Kaynak Göster
Yıl 2018, , 1466 - 1476, 01.10.2018
https://doi.org/10.16984/saufenbilder.402647

Öz

Kaynakça

  • [1] D. G. Hull, Fundamentals of Airplane Flight Mechanics. Heidelberg, Germany: Springer-Verlag Berlin, 2007.
  • [2] “Military Handbook Missile Part I Simulation One Surface-To-Air,” 1995.
  • [3] J. Roskam, “Airplane Flight Dynamics and Automatic Flight Controls – Part II,” USA, 2003.
  • [4] M. F. Hocaoglu, “AdSiF : Agent Driven Simulation Framework,” in Hunstville Simulation Conference -HSC2005, 2005.
  • [5] M. F. Hocaoğlu, “AdSiF : Agent driven Simulation Framework,” in USMOS 2011- National Defense Application and Modeling & Simulation Conference -(in Turkish), 2011.
  • [6] M. F. Hocaoğlu, “AdSiF: Developer Guide.” Agena Information & Defense System Ltd. www.agenabst.com, Istanbul, 2013.
  • [7] M. F. Hocaoğlu, “Aspect Oriented Programming Perspective in Agent Programming,” USMOS 2013- Natl. Def. Appl. Model. Simul. Conf. -(in Turkish), vol. 8, no. 3, 2013.
  • [8] M. F. Hocaoglu, “Aspect Oriented Programming Perspective in Software Agents and Simulation,” Int. J. Adv. Technol., vol. 8, no. 3, 2017.
  • [9] Wooldridge, M., An introduction to MultiAgent Systems. John Wiley & Sons, Ltd, 2002.
  • [10] R. J. Schalkoff, Artificial Intelligence: An Engineering Approach. McGraww-Hill, New York, 1990.
  • [11] D. J. Murray-Smith, Continuous System Simulation. University og Glasgow, Glasgow, UK: Chapman & Hall, 1995.

Agent-Based Dynamically Reconfigurable Missile Modelling

Yıl 2018, , 1466 - 1476, 01.10.2018
https://doi.org/10.16984/saufenbilder.402647

Öz



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).




Kaynakça

  • [1] D. G. Hull, Fundamentals of Airplane Flight Mechanics. Heidelberg, Germany: Springer-Verlag Berlin, 2007.
  • [2] “Military Handbook Missile Part I Simulation One Surface-To-Air,” 1995.
  • [3] J. Roskam, “Airplane Flight Dynamics and Automatic Flight Controls – Part II,” USA, 2003.
  • [4] M. F. Hocaoglu, “AdSiF : Agent Driven Simulation Framework,” in Hunstville Simulation Conference -HSC2005, 2005.
  • [5] M. F. Hocaoğlu, “AdSiF : Agent driven Simulation Framework,” in USMOS 2011- National Defense Application and Modeling & Simulation Conference -(in Turkish), 2011.
  • [6] M. F. Hocaoğlu, “AdSiF: Developer Guide.” Agena Information & Defense System Ltd. www.agenabst.com, Istanbul, 2013.
  • [7] M. F. Hocaoğlu, “Aspect Oriented Programming Perspective in Agent Programming,” USMOS 2013- Natl. Def. Appl. Model. Simul. Conf. -(in Turkish), vol. 8, no. 3, 2013.
  • [8] M. F. Hocaoglu, “Aspect Oriented Programming Perspective in Software Agents and Simulation,” Int. J. Adv. Technol., vol. 8, no. 3, 2017.
  • [9] Wooldridge, M., An introduction to MultiAgent Systems. John Wiley & Sons, Ltd, 2002.
  • [10] R. J. Schalkoff, Artificial Intelligence: An Engineering Approach. McGraww-Hill, New York, 1990.
  • [11] D. J. Murray-Smith, Continuous System Simulation. University og Glasgow, Glasgow, UK: Chapman & Hall, 1995.
Toplam 11 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Bilgisayar Yazılımı, Makine Mühendisliği, Endüstri Mühendisliği
Bölüm Araştırma Makalesi
Yazarlar

Mehmet Fatih Hocaoğlu 0000-0001-7428-9351

İlyas Kandemir 0000-0002-8773-6541

Yayımlanma Tarihi 1 Ekim 2018
Gönderilme Tarihi 6 Mart 2018
Kabul Tarihi 5 Temmuz 2018
Yayımlandığı Sayı Yıl 2018

Kaynak Göster

APA Hocaoğlu, M. F., & Kandemir, İ. (2018). Agent-Based Dynamically Reconfigurable Missile Modelling. Sakarya University Journal of Science, 22(5), 1466-1476. https://doi.org/10.16984/saufenbilder.402647
AMA Hocaoğlu MF, Kandemir İ. Agent-Based Dynamically Reconfigurable Missile Modelling. SAUJS. Ekim 2018;22(5):1466-1476. doi:10.16984/saufenbilder.402647
Chicago Hocaoğlu, Mehmet Fatih, ve İlyas Kandemir. “Agent-Based Dynamically Reconfigurable Missile Modelling”. Sakarya University Journal of Science 22, sy. 5 (Ekim 2018): 1466-76. https://doi.org/10.16984/saufenbilder.402647.
EndNote Hocaoğlu MF, Kandemir İ (01 Ekim 2018) Agent-Based Dynamically Reconfigurable Missile Modelling. Sakarya University Journal of Science 22 5 1466–1476.
IEEE M. F. Hocaoğlu ve İ. Kandemir, “Agent-Based Dynamically Reconfigurable Missile Modelling”, SAUJS, c. 22, sy. 5, ss. 1466–1476, 2018, doi: 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. https://doi.org/10.16984/saufenbilder.402647.
JAMA Hocaoğlu MF, Kandemir İ. Agent-Based Dynamically Reconfigurable Missile Modelling. SAUJS. 2018;22:1466–1476.
MLA Hocaoğlu, Mehmet Fatih ve İlyas Kandemir. “Agent-Based Dynamically Reconfigurable Missile Modelling”. Sakarya University Journal of Science, c. 22, sy. 5, 2018, ss. 1466-7, doi:10.16984/saufenbilder.402647.
Vancouver Hocaoğlu MF, Kandemir İ. Agent-Based Dynamically Reconfigurable Missile Modelling. SAUJS. 2018;22(5):1466-7.

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