Dynamic modeling of a multiple launch rocket system

Sert S., Taşcıoğlu Y.

2015 World Congress on Engineering, WCE 2015, London, İngiltere, 1 - 03 Temmuz 2015, cilt.2218, ss.1252-1256 identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Cilt numarası: 2218
  • Basıldığı Şehir: London
  • Basıldığı Ülke: İngiltere
  • Sayfa Sayıları: ss.1252-1256
  • Anahtar Kelimeler: Azimuth and elevation, Dynamic modeling, Electromechanical actuators, Multiple launch rocket system
  • TED Üniversitesi Adresli: Hayır

Özet

Multiple Rocket Launcher Systems (MLRS) are used to aim rockets to the desired elevation (pitch) and azimuth (yaw) angles in order to hit targets. In this paper, a dynamic model for an MLRS with electromechanical actuators is presented along with performance evaluation of four different friction models. The final model is simulated and the results are compared with the test data taken from the real MLRS. The results show that the proposed model is accurate within, on average, 5% of the actual system.