Study on dynamic decoupling design by using INA method for cruise missile

The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedbac...

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Main Authors: Xu, Jiangtao, Cui, Naigang, Tian, Jichao, Liu, Hongliang
Format: Conference Proceeding
Language:English
Subjects:
Aerospace control
Aircraft
Automatic control
Control systems
Feedback
Force control
Missiles
Nonlinear control systems
Space technology
Velocity control
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Cui, Naigang
Tian, Jichao
Liu, Hongliang
description The non-square model of cruise missile is strongly coupled between roll and yaw channels when the autopilot is design. Multi-variables coupling analysis is completed with a directive gain matrix for the non-square system. Then the non-square system is squared with coupling analysis and inner feedback. An extended dynamic decoupling method by using INA is presented for a dynamic pre-compensator design of a cruise missile non-square system. The mathematical simulation results indicate that the coupling effect is obviously weaken after using the dynamic decoupling compensator and drive a conclusion that the method is valid.
doi_str_mv 10.1109/ISSCAA.2008.4776389
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subjects Aerospace control
Aircraft
Automatic control
Control systems
Feedback
Force control
Missiles
Nonlinear control systems
Space technology
Velocity control
title Study on dynamic decoupling design by using INA method for cruise missile
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