Yerden Gelen Tehditlerden Kaçmak Amacıyla Düşük Hızlı Bir Hava Platformunun Yapabileceği Başlıca Manevraların İncelenmesi
Abstract
Yerden havaya doğru fırlatılan taşınabilir roket ve füzelerin tehdidi altındaki düşük hızlı ve karşı tedbir sistemi içermeyen helikopter ve insansız hava aracı gibi hava platformlarının bekasını sağlayabilmesi için yapması gereken en anlamlı hareket uygun bir manevrayla kaçmaktır. Bahsedilen yaklaşım, düşük hızlı platformların kapasitesini zorlayıcı bir özelliğe sahiptir. Bu çalışmada, düşük hızlı bir hava platformunun belirtilen kapsamda izleyebileceği belli başlı kaçma manevralarının etkinliği gerçekleştirilen bilgisayar benzetimleri yardımıyla incelenmektedir. Neticede, herhangi bir karşı tedbir olanağına sahip olmayan hava platformlarının yerden havaya fırlatılan mühimmattan kaçabileceği gösterilmektedir.
Keywords
Düşük Hızlı Hava Platformu İnsansız Hava Aracı Yerden Havaya Fırlatılan Tehdit Füze Manevra
References
- S. Chapman, The Next Generation in Aircraft Protection against Advanced MANPADS, 2014.
- W. Xin, L. Guofang, and X. Lizhong, X., “Infrared dim target detection based on visual attention”, Infrared Physics & Technology, vol. 55, pp. 513-521, 2012.
- B. Özkan, “Investigation of the kinematic performance characteristics of an antenna orientation mechanism utilized on a general-purpose aerial platform for threat detection (in Turkish)”, 18th National Machine Theory Symposium (UMTS2017), Karadeniz Technical University, Trabzon, Turkey, 2017.
- B. Özkan, M. K. Özgören and G. Mahmutyazıcıoğlu, “Comparison of the acceleration- and angle-based guidance laws for a short-range air-to-surface missile (in Turkish)”, Automatic Control National Meeting in 2008 (TOK2008), İstanbul Technical University, İstanbul, Turkey, 2008.
- B. Özkan, “Dynamic modeling, guidance, and control of homing missiles”, PhD Thesis, Middle East Technical University, Ankara, Turkey, 2005.
Investigation of the Notable Maneuvers of a Low-speed Air Platform to Get Away from Surface-to-Air Threats
Abstract
The most reasonable attitude in order for low-speed aerial platforms including helicopters and unmanned air vehicles which do not involve any counter measure system to survive is to get away with a convenient maneuver when they are subjected to man-portable surface-to-air rockets and missiles. The mentioned approach may become challenging for low-speed platforms. In this study, the effectiveness of notable escape maneuvers is investigated using relevant computer simulations for a low-speed aerial platform. This way, it is shown that the aerial platforms can escape from surface-to-air threats under the circumstance of lack of any counter measure opportunity.
References
- S. Chapman, The Next Generation in Aircraft Protection against Advanced MANPADS, 2014.
- W. Xin, L. Guofang, and X. Lizhong, X., “Infrared dim target detection based on visual attention”, Infrared Physics & Technology, vol. 55, pp. 513-521, 2012.
- B. Özkan, “Investigation of the kinematic performance characteristics of an antenna orientation mechanism utilized on a general-purpose aerial platform for threat detection (in Turkish)”, 18th National Machine Theory Symposium (UMTS2017), Karadeniz Technical University, Trabzon, Turkey, 2017.
- B. Özkan, M. K. Özgören and G. Mahmutyazıcıoğlu, “Comparison of the acceleration- and angle-based guidance laws for a short-range air-to-surface missile (in Turkish)”, Automatic Control National Meeting in 2008 (TOK2008), İstanbul Technical University, İstanbul, Turkey, 2008.
- B. Özkan, “Dynamic modeling, guidance, and control of homing missiles”, PhD Thesis, Middle East Technical University, Ankara, Turkey, 2005.
Details
| Primary Language | English |
|---|---|
| Subjects | Engineering |
| Journal Section | Articles |
| Authors | |
| Publication Date | November 30, 2021 |
| Published in Issue | Year 2021 Issue: 28 |
