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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 1: 57 - 59

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.01.037

MISSILES AND GUIDANCE TECHNOLOGY

The Design and Simulation of the Control System for a Guided Rocket

  • WANG Jinzhu ,
  • LV Shuai ,
  • ZHANG Ming ,
  • GUO Rihong
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  • 1 Ordnance Engineering College, Shijiazhuang 050003, China
    2 Military Representative Office in Huludao Area, Liaoning Huludao 125125, China
    3 Ordnance Technology Institute, Shijiazhuang 050000, China

Received date: 2011-03-15

  Online published: 2025-05-29

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Abstract

In order to design the control system for a guided rocket and ensure that it takes on favorable dynamic performance, the design and simulation of the control system was described. The mathematical model of the rocket was established on the basis of its motion equations, from which the transfer function of the body was deduced. Small disturbance precondition and frozen coefficient method were used in the process of derivation. Then the simulation model was built under Simulink environment, and the parameters of the control system were optimized by using Signal Constraint Module. The simulation results indicate that the control system works well and lays a foundation for further research.

Key words： guided rocket; control system; simulation; dynamic performance

Cite this article

WANG Jinzhu , LV Shuai , ZHANG Ming , GUO Rihong . The Design and Simulation of the Control System for a Guided Rocket[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(1) : 57 -59 . DOI: 10.15892/j.cnki.djzdxb.2012.01.037

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