Dynamic Modeling of a Multiple Launch Rocket System

Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/1557

Title:	Dynamic Modeling of a Multiple Launch Rocket System
Authors:	Sert, Serdar Taşcıoğlu, Yiğit
Keywords:	azimuth and elevation dynamic modeling electromechanical actuators multiple launch rocket system
Publisher:	Int Assoc Engineers-Iaeng
Source:	Jitpraphai, T., & Costello, M. (2001). Dispersion reduction of a direct fire rocket using lateral pulse jets. Journal of Spacecraft and Rockets, 38(6), 929-936.
Abstract:	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.
URI:	https://doi.org/10.2514/2.3765 https://hdl.handle.net/20.500.11851/1557
ISBN:	978-988-14047-0-1
ISSN:	2078-0958
Appears in Collections:	Makine Mühendisliği Bölümü / Department of Mechanical Engineering Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

CORE Recommender

1

checked on Aug 31, 2024

164

checked on Dec 23, 2024

Check