Research Article
BibTex RIS Cite

Guidance and Control of a Surface-to-Surface Projectile Using a Nose Actuation Kit

Year 2021, Issue: 22, 282 - 292, 31.01.2021
https://doi.org/10.31590/ejosat.848994

Abstract

Surface-to-surface projectiles are fired from ground launchers to specified ground targets to destroy them in an effective and economical manner. The mentioned munition is usually unguided and thus follows a ballistic trajectory. However, it is inevitable to have large miss distances when the diverting effects of the wind and thrust uncertainty are apparent. In this study, a gradual guidance and control strategy is proposed to improve the performance of this kind of munition. The effectiveness of this approach is shown by means of relevant computer simulations. The use of a simpler and cheaper nose actuation kit with pneumatic actuation makes this approach a preferable option for the application.

References

  • F. Fresconi, G. Cooper, I. Celmins, J. DeSpirito, M. Costello: Flight mechanics of a novel guided spin-stabilized projectile concept, Proc. IMechE, Part G: Journal of Aerospace Engineering, 226(2011), 327-340.
  • F. Fresconi, I. Celmins, Experimental Flight Characterization of Spin-Stabilized Projectiles at High Angle of Attack, US Army Research Laboratory Report, USA, 2017.
  • M. D. Ilg, Guidance, Navigation, and Control for Munitions, PhD Thesis, Drexel University, USA, 2008.
  • J. Rogers, M. Costello: Design of a roll-stabilized mortar projectile with reciprocating canards, Journal of Guidance, Control, and Dynamics, 33-4(2010), 1026-1034.
  • Y. Qing, L. Chunsheng: A differential game-based guidance law for an accelerating exoatmospheric missile, Asian Journal of Control, 19-3(2017), 1205–1216.
  • G. Jiwei, C. Yuan-Li Cai: Three-dimensional impact angle constrained guidance laws with fixed-time convergence, Asian Journal of Control, 19-6(2017), 2240–2254.
  • M. Eroğlu, Design and Control of Nose Actuation Kit for Position Correction of Spin Stabilized Munitions under Wind Effect, MSc Thesis, Middle East Technical University, Ankara, Turkey, 2016.
  • Y. Habash: Roll controlled guided mortar (RCGM), NDIA Joint Armaments Conference, Seattle, WA, USA, 2012.
  • D. N. Gkritzapis, D. P. Margaris, E. E. Panagiotopoulos, G. Kaimakamis, K. Siassiakos: Prediction of the impact point for a spin and fin-stabilized projectiles, WSEAS Transactions on Information Science and Applications, 5-12(2008), 1667-1676.
  • D. N. Gkritzapis, E. E. Panagiotopoulos, D. P. Margaris, D. G. Papanikas: Modified linear theory for spinning or non-spinning projectiles, The Open Mechanics Journal, 6-11(2008), 6-11.
  • L. Baranowski: Equations of motion of a spin-stabilized projectile for flight stability testing, Journal of Theoretical and Applied Mechanics, 51-1(2013), 235-246.
  • J. Yin, X. Wu, J. Lei, T. Lu, X. Liu: Canard interference on the Magnus effect of a fin-stabilized spinning missile, Advances in Mechanical Engineering, 10-7(2018), 1-16.
  • B. Özkan: Dynamic modelling of spin-stabilized projectiles (in Turkish), 19th National Theory of Machine Symposium, İskenderun Technical University, İskenderun, Hatay, Turkey, 2019.
  • G. R. Cooper, M. Costello: Trajectory prediction of spin-stabilized projectiles with a liquid payload, Journal of Spacecraft and Rockets, 48-4(2011), 664-670.
  • K. D. Şahin, A Pursuit Evasion Game between an Aircraft and a Missile, MSc Thesis, Middle East Technical University, Ankara, Turkey, 2002.
  • B. Özkan, M. K. Özgören, G. Mahmutyazıcıoğlu: Modeling of dynamics, guidance, and control systems of air-to-surface missiles, The Journal of Defense Modeling and Simulation: Applications, Methodology, Technology, 9-2(2012), 101-112.
  • M. Milinović, D. Jerković, O. Jeremić, M. Kovač: Experimental and simulation testing of flight spin stability for small calibre cannon projectile: Journal of Mechanical Engineering, 58-6(2012), 394-402.

Karadan Karaya Bir Merminin Burun Eyletim Kiti Kullanılarak Güdüm ve Denetimi

Year 2021, Issue: 22, 282 - 292, 31.01.2021
https://doi.org/10.31590/ejosat.848994

Abstract

Etkili ve ekonomik bir şekilde yok etmek için satıhtan satha füzeler yer rampalarından belirlenen yer hedeflerine ateşlenir. Bahsedilen mühimmat genellikle güdümsüzdür ve bu nedenle balistik bir yörünge izler. Bununla birlikte, rüzgarın ve itme belirsizliğinin yön değiştirici etkilerinin açık olduğu durumlarda büyük ıskalama mesafelerine sahip olmak kaçınılmazdır. Bu çalışmada, bu tür mühimmatın performansını artırmak için aşamalı bir rehberlik ve kontrol stratejisi önerilmiştir. Bu yaklaşımın etkinliği, ilgili bilgisayar simülasyonları aracılığıyla gösterilmiştir. Pnömatik çalıştırmalı daha basit ve daha ucuz bir burun çalıştırma kitinin kullanılması, bu yaklaşımı uygulama için tercih edilen bir seçenek haline getirir.

References

  • F. Fresconi, G. Cooper, I. Celmins, J. DeSpirito, M. Costello: Flight mechanics of a novel guided spin-stabilized projectile concept, Proc. IMechE, Part G: Journal of Aerospace Engineering, 226(2011), 327-340.
  • F. Fresconi, I. Celmins, Experimental Flight Characterization of Spin-Stabilized Projectiles at High Angle of Attack, US Army Research Laboratory Report, USA, 2017.
  • M. D. Ilg, Guidance, Navigation, and Control for Munitions, PhD Thesis, Drexel University, USA, 2008.
  • J. Rogers, M. Costello: Design of a roll-stabilized mortar projectile with reciprocating canards, Journal of Guidance, Control, and Dynamics, 33-4(2010), 1026-1034.
  • Y. Qing, L. Chunsheng: A differential game-based guidance law for an accelerating exoatmospheric missile, Asian Journal of Control, 19-3(2017), 1205–1216.
  • G. Jiwei, C. Yuan-Li Cai: Three-dimensional impact angle constrained guidance laws with fixed-time convergence, Asian Journal of Control, 19-6(2017), 2240–2254.
  • M. Eroğlu, Design and Control of Nose Actuation Kit for Position Correction of Spin Stabilized Munitions under Wind Effect, MSc Thesis, Middle East Technical University, Ankara, Turkey, 2016.
  • Y. Habash: Roll controlled guided mortar (RCGM), NDIA Joint Armaments Conference, Seattle, WA, USA, 2012.
  • D. N. Gkritzapis, D. P. Margaris, E. E. Panagiotopoulos, G. Kaimakamis, K. Siassiakos: Prediction of the impact point for a spin and fin-stabilized projectiles, WSEAS Transactions on Information Science and Applications, 5-12(2008), 1667-1676.
  • D. N. Gkritzapis, E. E. Panagiotopoulos, D. P. Margaris, D. G. Papanikas: Modified linear theory for spinning or non-spinning projectiles, The Open Mechanics Journal, 6-11(2008), 6-11.
  • L. Baranowski: Equations of motion of a spin-stabilized projectile for flight stability testing, Journal of Theoretical and Applied Mechanics, 51-1(2013), 235-246.
  • J. Yin, X. Wu, J. Lei, T. Lu, X. Liu: Canard interference on the Magnus effect of a fin-stabilized spinning missile, Advances in Mechanical Engineering, 10-7(2018), 1-16.
  • B. Özkan: Dynamic modelling of spin-stabilized projectiles (in Turkish), 19th National Theory of Machine Symposium, İskenderun Technical University, İskenderun, Hatay, Turkey, 2019.
  • G. R. Cooper, M. Costello: Trajectory prediction of spin-stabilized projectiles with a liquid payload, Journal of Spacecraft and Rockets, 48-4(2011), 664-670.
  • K. D. Şahin, A Pursuit Evasion Game between an Aircraft and a Missile, MSc Thesis, Middle East Technical University, Ankara, Turkey, 2002.
  • B. Özkan, M. K. Özgören, G. Mahmutyazıcıoğlu: Modeling of dynamics, guidance, and control systems of air-to-surface missiles, The Journal of Defense Modeling and Simulation: Applications, Methodology, Technology, 9-2(2012), 101-112.
  • M. Milinović, D. Jerković, O. Jeremić, M. Kovač: Experimental and simulation testing of flight spin stability for small calibre cannon projectile: Journal of Mechanical Engineering, 58-6(2012), 394-402.
There are 17 citations in total.

Details

Primary Language English
Subjects Engineering
Journal Section Articles
Authors

Bülent Özkan 0000-0003-3112-9723

Harun Gökçe 0000-0002-2702-0111

Publication Date January 31, 2021
Published in Issue Year 2021 Issue: 22

Cite

APA Özkan, B., & Gökçe, H. (2021). Guidance and Control of a Surface-to-Surface Projectile Using a Nose Actuation Kit. Avrupa Bilim Ve Teknoloji Dergisi(22), 282-292. https://doi.org/10.31590/ejosat.848994