The PID Control Stability Analysis and Simulation of Missile Posture Inner Loop Based on Simulink-Reference-Cited by-同舟云学术

The PID Control Stability Analysis and Simulation of Missile Posture Inner Loop Based on Simulink

Published:2014-09 Issue: Volume:644-650 Page:150-153
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Peng Jun¹,Lei Jun Wei¹,Liu Di¹

Affiliation:

1. Naval Aeronautical and Astronautical University

Abstract

For posture angle tracking problem of missile pitch channel linear model, PID controller is designed. Programming implementation issues is studied based on simulink. The open-loop transfer function calculation method which contains PID controller is put forward by using matlab. The bode diagram of system is worked out. The judgment method of analysing system stability is put forward based on simulink.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.644-650.150.pdf

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