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

Jun Peng; Jun Wei Lei; Di Liu

doi:10.4028/www.scientific.net/AMM.644-650.150

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650The PID Control Stability Analysis and Simulation...

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

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.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

150-153

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.150

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Online since:

September 2014

Authors:

Jun Peng*, Jun Wei Lei, Di Liu

Keywords:

Attitude Angle, Control System, Inner Loop, Missile, Stability

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