Dynamic Modeling of a Multiple Launch Rocket System

被引：0
|
作者：
Sert, Serdar [1 ,2 ]
Tascioglu, Yigit [3 ]
机构：
[1] Roketsan AS, TR-06780 Ankara, Turkey
[2] TOBB Univ Econ & Technol, TR-06590 Ankara, Turkey
[3] TOBB Univ Econ & Technol, Dept Mech Engn, TR-06590 Ankara, Turkey
来源：
WORLD CONGRESS ON ENGINEERING, WCE 2015, VOL II | 2015年
关键词：
azimuth and elevation; dynamic modeling; electromechanical actuators; multiple launch rocket system;
D O I：
暂无
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
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.
引用
收藏
页码：1252 / +
页数：3
相关论文
共 50 条
  • [21] Design and implementation of an adaptive Kalman filtering for the launcher of multiple launch rocket system
    Li, Bo
    Rui, Xiaoting
    Yang, Fufeng
    Wang, Guoping
    INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING, 2018, 32 (03) : 447 - 463
  • [22] Modeling and Simulation for Dynamic System of Electromagnetic Aircraft Launch
    Zhu, Xiaoming
    Li, Haixu
    Qu, Xiangju
    CONFERENCE PROCEEDINGS OF 2017 3RD IEEE INTERNATIONAL CONFERENCE ON CONTROL SCIENCE AND SYSTEMS ENGINEERING (ICCSSE), 2017, : 125 - 129
  • [23] Dynamics design for multiple launch rocket system using transfer matrix method for multibody system
    Tang, Wenbing
    Rui, Xiaoting
    Wang, Guoping
    Rui, Xue
    Song, Zhendong
    Gu, Lilin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (14) : 2557 - 2568
  • [24] Launch dynamic modeling and simulation analysis of a multi-rocket launch system With rigid-flexible coupled and rigid body-liquid coupled methods
    Feng, Y., 1600, Chinese Vibration Engineering Society (33):
  • [25] Modeling and Dynamic Analysis of a Rocket Towed Net System
    Han F.
    Zhou Q.
    Chen F.
    Binggong Xuebao/Acta Armamentarii, 2019, 40 (09): : 1836 - 1848
  • [26] Study on simulation and experiment of control for multiple launch rocket system by computed torque method
    Li, Bo
    Rui, Xiaoting
    Zhou, Qinbo
    NONLINEAR DYNAMICS, 2018, 91 (03) : 1639 - 1652
  • [27] Vibration characteristics of airborne multiple launch rocket systems
    Institute of Launch Dynamics, Nanjing University of Science and Technology, Nanjing 210094, China
    Zhendong Gongcheng Xuebao, 2013, 1 (15-19):
  • [28] Study on simulation and experiment of control for multiple launch rocket system by computed torque method
    Bo Li
    Xiaoting Rui
    Qinbo Zhou
    Nonlinear Dynamics, 2018, 91 : 1639 - 1652
  • [29] Automatic Optical Tracking System for Rocket Launch
    Curetti, Maria
    Garcia Bravo, Santiago
    Mathe, Ladislao
    2014 IEEE BIENNIAL CONGRESS OF ARGENTINA (ARGENCON), 2014, : 304 - 309
  • [30] Trajectory Design of a Rocket-Scramjet-Rocket Multistage Launch System
    Forbes-Spyratos, Sholto O.
    Kearney, Michael P.
    Smart, Michael K.
    Jahn, Ingo H.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2019, 56 (01) : 53 - 67
12345