1. DergiPark
  2. Anadolu Üniversitesi Bilim Ve Teknoloji Dergisi A - Uygulamalı Bilimler ve Mühendislik
  3. Arşiv
  4. Cilt 18, Sayı 4
Yıl 2017, Cilt 18 , Sayı 4, Sayfalar 788 - 803 2017-10-31

PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY

Hamza KAMİŞLİ [1] , Metin U. SALAMCI [2] , Bülent ÖZKAN [3]

Öz

Dynamic modeling and control of two-degree-of-freedom launchers which are utilized for launching munitions such as missiles and rockets have become one of the most popular fields in recent years. Control of launch vehicles gains more importance especially when they are mounted on moving vehicles. In this study, the mathematical modeling and control with parameter uncertainties of a high-accuracy two-degree-of-freedom electromechanically-actuated launcher are investigated in the direction of reducing the impact impulse on the control system. In this context, after the dynamic equations of the system are derived, the design of convenient control systems is carried out so as to reduce the undesired contribution of the thrust effect. In control, computed torque and proportional, integral, and derivative (PID) and computed torque and sliding mode control algorithms, and computed torque and sliding mode control cascaded control algorithms are developed by taking the parameter uncertainties into consideration. In the conclusion part, the performance characteristics of these controllers are compared and it is shown that the cascaded control scheme yields more satisfactory results in accurate position control. In the computer simulations conducted in this extent, the MATLABÒ software and its SIMULINKÒ module are utilized.

Anahtar Kelimeler

Electromechanically-actuated launcher, launcher control, computed torque, sliding mode, parameter uncertainty

Kaynakça

  • [1] Kamişli H. Design of control systems for a launcher to reduce the thrust effect (thesis in Turkish with an abstract in English). MSc, Gazi University, Ankara, Turkey, 2015.
  • [2] Haug D, Wagner H. Active hardkill protection systems: analysis and evaluation of different system concepts. Technical Report, 2011.
  • [3] Zhang D, Xiao J. A dynamic model for rocket launcher with coupled rigid and flexible motion. Applied Mathematics and Mechanics 2005; 26: 5: 609-617.
  • [4] Dziopa Z, Krzysztofik I, Koruba Z. An analysis of the dynamics of a launcher-missile system on a movable base. Bulletin of the Polish Academy of Sciences, Technical Sciences, 2010; 58: 4: 645-650.
  • [5] Bingül Z, Küçük S. Robot Dinamiği ve Kontrolü. İstanbul, Turkey: Birsen Yayınevi, 2008.
  • [6] Dokumacı K. Mathematical modelling, PID and sliding mode control of a rocket launcher system. MSc, Gazi University, Ankara, Turkey, 2014. [7] Kamişli H, Salamci MU, Özkan B. Elektromekanik eyletimli bir firlatma sisteminin itki etkisini en aza indirgeyecek şekilde denetimi. Otomatik Kontrol Ulusal Toplantısı (TOK), Denizli, Turkey, 2015.
  • [8] Utkin VI. Sliding Mode Control. Encylopedia of Life Support Systems (EOLSS), Control Systems, Robotics and Automation. Vol XIII, 2009.
  • [9] Utkin V, Guldner J, Shi J. Sliding Mode Control in Electromechanical Systems. USA: Taylor and Francis, 103-153, 271-302, 2009.
  • [10] Özkan B. Dynamic modeling and control of an electromechanically-actuated launcher (proceeding in Turkish with an abstract in English). Ulusal Makine Teorisi Sempozyumu, Erzurum, Turkey, 2013.
  • [11] Kamişli H, Salamci MU, Özkan B. Dynamic modeling of an electromechanically-actuated launcher. 17th International Carpathian Control Conference, Slovakia, 2016.
  • [12] Kamişli H, Salamci MU, Özkan B. Design of a cascaded control system for an electromechanically-actuated launcher to reduce the thrust effect. 17th International Carpathian Control Conference, Slovakia, 2016.
  • [13] Ogata K. Modern Control Engineering. 5th ed. New Jersey, USA: Pearson, 2010.

Ayrıntılar

Konular Mühendislik
Bölüm Araştırma Makalesi
Yazarlar

Yazar: Hamza KAMİŞLİ

Yazar: Metin U. SALAMCI

Yazar: Bülent ÖZKAN
Kurum: Türkiye Bilimsel ve Teknolojik Araştırma Kurumu, SAGE
Ülke: Turkey
Tarihler

Yayımlanma Tarihi : 31 Ekim 2017

Kaynak Göster

Bibtex @araştırma makalesi { aubtda340842, journal = {Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering}, issn = {1302-3160}, eissn = {2146-0205}, address = {}, publisher = {Eskişehir Teknik Üniversitesi}, year = {2017}, volume = {18}, pages = {788 - 803}, doi = {10.18038/aubtda.340842}, title = {PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY}, key = {cite}, author = {Kami̇şli̇, Hamza and Salamcı, Metin U. and Özkan, Bülent} }
APA Kami̇şli̇, H , Salamcı, M , Özkan, B . (2017). PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY . Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering , TOK2016 ÖZEL SAYISI , 788-803 . DOI: 10.18038/aubtda.340842
MLA Kami̇şli̇, H , Salamcı, M , Özkan, B . "PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY" . Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 18 (2017 ): 788-803 <https://dergipark.org.tr/tr/pub/aubtda/issue/31353/340842>
Chicago Kami̇şli̇, H , Salamcı, M , Özkan, B . "PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY". Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 18 (2017 ): 788-803
RIS TY - JOUR T1 - PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY AU - Hamza Kami̇şli̇ , Metin U. Salamcı , Bülent Özkan Y1 - 2017 PY - 2017 N1 - doi: 10.18038/aubtda.340842 DO - 10.18038/aubtda.340842 T2 - Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering JF - Journal JO - JOR SP - 788 EP - 803 VL - 18 IS - 4 SN - 1302-3160-2146-0205 M3 - doi: 10.18038/aubtda.340842 UR - https://doi.org/10.18038/aubtda.340842 Y2 - 2017 ER -
EndNote %0 Anadolu Üniversitesi Bilim Ve Teknoloji Dergisi A - Uygulamalı Bilimler ve Mühendislik PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY %A Hamza Kami̇şli̇ , Metin U. Salamcı , Bülent Özkan %T PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY %D 2017 %J Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering %P 1302-3160-2146-0205 %V 18 %N 4 %R doi: 10.18038/aubtda.340842 %U 10.18038/aubtda.340842
ISNAD Kami̇şli̇, Hamza , Salamcı, Metin U. , Özkan, Bülent . "PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY". Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering 18 / 4 (Ekim 2017): 788-803 . https://doi.org/10.18038/aubtda.340842
AMA Kami̇şli̇ H , Salamcı M , Özkan B . PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY. AUBTD-A. 2017; 18(4): 788-803.
Vancouver Kami̇şli̇ H , Salamcı M , Özkan B . PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY. Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering. 2017; 18(4): 788-803.
IEEE H. Kami̇şli̇ , M. Salamcı ve B. Özkan , "PRECISE CONTROL OF AN ELECTROMECHANICALLY-ACTUATED LAUNCHER UNDER PARAMETER UNCERTAINTY", Anadolu University Journal of Science and Technology A - Applied Sciences and Engineering, c. 18, sayı. 4, ss. 788-803, Eki. 2017, doi:10.18038/aubtda.340842
Makalenin Yazarları
Hamza KAMİŞLİ [1]
Metin U. SALAMCI [2]
Bülent ÖZKAN [3]
Arşiv
Editör Kurulu
İletişim
TR Dizin
TR Dizin